Papers
Participants can find their papers with the EUCASS Search Engine
The conference has been held using five parallel symposia dealing with aspects of:
- SI SYSTEM INTEGRATION on Aircraft and Space Launch Vehicles
- FP FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re- Entry Bodies
- SM STRUCTURES AND MATERIALS for Aeronautics and Space Systems
- FD FLIGHT DYNAMICS/ GNC and AVIONICS for Aeronautics and Space Applictions
- PP PROPULSION PHYSICS for Air-Breathing and Rocket Engines
A poster session was present as well.
Here you find the full papers from the main sessions and the poster session with their respective DOI and the link to the paper published in open access.
They have been organized in cronological order according to each respective session.
A few plenary presentations are available as well in pdf format.
Plenary Presentations
- Stéphane Andrieux, ONERA, Transdisciplinary Research Policy for Preparing the Future?
- Filippo Graziani, GAUSS, Micro & Nano Satellites. Present and Future
- Gérald Carrier, ONERA, Innovative Engine Integration Solutions for Transport Aircraft : Current Research and Future Challenges
- L. Wiart, O. Atinault, D. Hue, R. Grenon, B. Paluch, ONERA, Development of NOVA Aircraft Configurations for Large Engine Integration Studies
- Christophe Bonnal, CNES, Sustainable activities in space: Space debris problematic in a nutshell
- Jan Wörner, European Space Agency, EURO(PE) and SPACE
Full Papers
FD - Optimization
- DOI: 10.13009/EUCASS2017-71 - New improvements in the optimization of the launcher ascent trajectory through the HJB approach
- DOI: 10.13009/EUCASS2017-254 - Optimal Aircraft Path Planning Considering Wind Uncertainty
- DOI: 10.13009/EUCASS2017-338 - Optimization of WIG-craft 3D-trajectory near the rough sea surface
- DOI: 10.13009/EUCASS2017-463 - On the minimum time optimal control problem of an aircraft in its climbing phase
- DOI: 10.13009/EUCASS2017-137 - Optimal Scheduling Algorithm in Point Merge System Including Holding Pattern Based on MILP
- DOI: 10.13009/EUCASS2017-498 - The control optimization of low-orbit spacecraft with electric ramjet
- DOI: 10.13009/EUCASS2017-545 - Trajectory Optmization of Commom Aero Vehicle through Genetic Algorithm aided with Rational Bezier Curve
FP - CFD I
- DOI: 10.13009/EUCASS2017-181 - Computationally expensive aerodynamic design optimization framework with adaptive search strategies and data fusion
- DOI: 10.13009/EUCASS2017-215 - Micro-Aerothermodynamics Analysis of the SpaceLiner Cabin Escape System along Atmospheric Re-entry
- DOI: 10.13009/EUCASS2017-226 - Aerodynamic Database Improvement of Aircrafts based on Neural Networks and Genetic Algorithms
- DOI: 10.13009/EUCASS2017-353 - A hybrid LST-RANS method for modeling of laminar-turbulent transition
- DOI: 10.13009/EUCASS2017-689 - DSMC Computations of Leading-Edge Separation in Hypersonic Flows
FP - Computational and Experimental Aerodynamics of Air Vehicules II
- DOI: 10.13009/EUCASS2017-416 - Aeroshape Trade-Off and Aerodynamic Analysis of the Space-Rider Vehicle
- DOI: 10.13009/EUCASS2017-424 - Experimental Research of the Inward-Turning Intake Starting at TsAGI T-116 Wind Tunnel within the International HEXAFLY-INT Project
- DOI: 10.13009/EUCASS2017-445 - Conceptual Design of Distributed Propeller Aircraft: Linear Aerodynamic Model Verification of Propeller-Wing Interaction
- DOI: 10.13009/EUCASS2017-447 - Wing geometric parameter studies of a box wing aircraft configuration for subsonic flight
- DOI: 10.13009/EUCASS2017-450 - An optimization study for fuselage layout of a regional jet
- DOI: 10.13009/EUCASS2017-651 - Numerical and Experimental Investigation of Ducted Fans Interference for Multirotor Copter-type Aerial Vehicle
- DOI: 10.13009/EUCASS2017-657 - Experimental study of the effects of exhaust plume and nozzle length on transonic and supersonic axisymmetric base flows
- DOI: 10.13009/EUCASS2017-108 - Aerodynamic Data Fusion with a Multi-fidelity Surrogate Modeling Method
FP - Rarefield and Real Gas Flows I
- DOI: 10.13009/EUCASS2017-66 - On orbit contaminant deposition measurements on Russian orbital stations and on the Russian segment of the International Space Station
- DOI: 10.13009/EUCASS2017-111 - State-resolved models of chemical reactions for non-equilibrium flow simulations
- DOI: 10.13009/EUCASS2017-199 - State-to-state models of physico-chemical processes in Direct Simulation Monte Carlo (DSMC) computations of 2-dimensional flows
FP - Wind Tunnel and Measurement Techniques I
- DOI: 10.13009/EUCASS2017-155 - Experimental Investigation of the VKI Longshot Gun Tunnel Compression Process
- DOI: 10.13009/EUCASS2017-168 - Mach 3 Turbulent Boundary Layer Measurement over a Flat Plate Using the Particle Image Velocimetry
- DOI: 10.13009/EUCASS2017-186 - Sub-scale hypersonic free flight dynamics of HEXAFLY-INT EFTV + ESM (multibody separation)
- DOI: 10.13009/EUCASS2017-187 - Wind tunnel test comparison between JAXA-HIEST and ONERA-S4MA with HYFLEX lifting-body
PP - Green liquid propellants I
- DOI: 10.13009/EUCASS2017-319 - Technology development for ADN-based green monopropellant thrusters - an overview of the Rheform project
- DOI: 10.13009/EUCASS2017-639 - Challenges and Economic Benefits of Green Propellants for Satellite Propulsion
- DOI: 10.13009/EUCASS2017-479 - Development of catalytic materials for decomposition of ADN-based monopropellants
- DOI: 10.13009/EUCASS2017-143 - Preliminary Tests on Thermal Ignition of ADN-based Liquid Monopropellants
- DOI: 10.13009/EUCASS2017-618 - A Numerical Study of the Time Dependent Combustion of a Gel Fuel Droplet
PP - LRE I
- DOI: 10.13009/EUCASS2017-418 - Development History and Verification of the Flight Model of a 500 N Ethanol/LOX Rocket Engine
- DOI: 10.13009/EUCASS2017-248 - EUCASS 2017 248 Overview of FLPP Propulsion Projects Final
- DOI: 10.13009/EUCASS2017-474 - Nitrous Oxide Application for Low-Thrust and Low-Cost Liquid Rocket Engine
- DOI: 10.13009/EUCASS2017-627 - PERSEUS Project 5kN LOX/Ethanol rocket engine fire tests
- DOI: 10.13009/EUCASS2017-282 - DESIGN, MANUFACTURE, ASSEMBLY AND TESTING OF A LIQUID (LOX AND GASOLINE) ROCKET MOTOR FOR A VEHICLE WITH STRATOSPHERIC APOGEE IN COLOMBIA: THE SUA II ENGINE
- DOI: 10.13009/EUCASS2017-503 - BOREAS DEMONSTRATOR FOR FUTURE LIQUID PROPULSION ENGINES
- DOI: 10.13009/EUCASS2017-227 - Flow visualization of the priming process in spacecraft feedlines
PP - LRE chamber cooling
- DOI: 10.13009/EUCASS2017-649 - Preliminary Study on Wall-modeled Large Eddy Simulation of Turbulent Heat Transfer for Liquid Rocket Engines
- DOI: 10.13009/EUCASS2017-589 - Numerical Simulation of Turbulent Boundary Layers with Foreign Gas Transpiration using OpenFOAM
- DOI: 10.13009/EUCASS2017-453 - 2D Thermo-Structural Code Development for Regenerative Combustion Chamber Analysis
- DOI: 10.13009/EUCASS2017-260 - Experimental analysis of heat transfer in cryogenic combustion chambers on Mascotte test bench
- DOI: 10.13009/EUCASS2017-331 - SIMULATION OF NONEQUILIBRIUM HYDROCARBON GAS FLOW IN THE HIGH ASPECT RATIO CHANNELS WITH PHASE TRANSITION AND HIGH HEAT INTENSITY
- DOI: 10.13009/EUCASS2017-476 - Numerical investigation of transpiration cooling with uniformly and non-uniformly simulated injection
PP - Liquid combustion
- DOI: 10.13009/EUCASS2017-369 - Response of a Transcritical Coaxial Flame to Propellant Injection Rate Modulations: Analysis and Low-Order Modeling of the Generation of Unsteady Heat Release Rate
- DOI: 10.13009/EUCASS2017-247 - Large-eddy simulation of multi-element LOx/H2 combustion at transcritical conditions
- DOI: 10.13009/EUCASS2017-588 - Solution of a droplet combustion process using modified thermal resistors model
- DOI: 10.13009/EUCASS2017-609 - Analysis of coaxial-flame response during transverse combustion instability
- DOI: 10.13009/EUCASS2017-395 - Evaluation of the Grid Convergence for a Rocket Combustion Chamber with a Porous Injector
- DOI: 10.13009/EUCASS2017-608 - Modeling scalar mixing and transport in LRE-like conditions
PP - Nozzles and plumes I
- DOI: 10.13009/EUCASS2017-359 - The TICTOP nozzle - first experimental results
- DOI: 10.13009/EUCASS2017-666 - Effect of non-circular nozzle shape on impingement cooling characteristics
- DOI: 10.13009/EUCASS2017-523 - Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Application of Quasi-1D engineering models and 2D axisymmetric CFD
PP - Test benches and diagnostics
- DOI: 10.13009/EUCASS2017-234 - 50 Years of Test Complex M11 in Lampoldshausen - Research on Space Propulsion Systems for Tomorrow
- DOI: 10.13009/EUCASS2017-198 - Test Bench for Key Components of Megawatt Class International Power and Propulsion System Ground Demonstration
- DOI: 10.13009/EUCASS2017-225 - PERGOLA: an experimental facility to investigate storable propellants' combustion
- DOI: 10.13009/EUCASS2017-388 - DESIGN OF A CANDY PROPELLANT ROCKET MOTOR BY A COMPUTER AIDED SYSTEM AND ITS PERFORMANCE IN STATIC TESTING
- DOI: 10.13009/EUCASS2017-437 - The pressure dependence of optical flame emission from space propulsion-relevant hydrogen combustion
- DOI: 10.13009/EUCASS2017-375 - Active flow control by means of plasma actuator in the curvilinear channel
SI - Aircraft System Concept and MDO
- DOI: 10.13009/EUCASS2017-20 - A Systems Engineering Approach to Variable Intakes for Civil Aviation
- DOI: 10.13009/EUCASS2017-246 - Integrated equipment installation and optimisation for new engine architecture nacelles
- DOI: 10.13009/EUCASS2017-373 - Configuration Design and Optimization of Ducted Fan Using Parameter Based Design
- DOI: 10.13009/EUCASS2017-209 - Conceptual Design of Self-Expanding Folding Extremely Large Aspect Ratio Wing Airplane
- DOI: 10.13009/EUCASS2017-271 - A Modelling and Simulation Framework for the Integrated Design of Aircraft Systems
- DOI: 10.13009/EUCASS2017-280 - Motor mass optimization for the maximization of solar-powered aircraft performance
- DOI: 10.13009/EUCASS2017-676 - Advances, Challenges and Future of All Electric Aircraft-Jose Posada
SI/FD - Rendez-vous and Debris
- DOI: 10.13009/EUCASS2017-317 - GNC architecture for the e.Deorbit mission
- DOI: 10.13009/EUCASS2017-632 - On Ground Validation of Debris Removal technologies
- DOI: 10.13009/EUCASS2017-612 - Contact Dynamic Models of Space Debris Capturing Using A Net
- DOI: 10.13009/EUCASS2017-631 - SBSS-DM and ANDROID: two small missions for Space-Based Space Surveillance and Active Debris Removal Demonstrations
- DOI: 10.13009/EUCASS2017-47 - Service Spacecraft Control During the Space Debris Removal from the GEO Protection Region by the Ion Shepherd Method
SM - Advanced Materials/Technologies I
- DOI: 10.13009/EUCASS2017-252 - Investigations on microstructure and mechanical properties of non-flammable Mg-Al-Zn-Ca-Y extruded alloys
- DOI: 10.13009/EUCASS2017-633 - AlMgSc alloy 5028 status of maturation
- DOI: 10.13009/EUCASS2017-131 - FLPP ETID: Enabling Technologies for Future European Upper Stage Engines
FD - Aerodynamic modelling and identification
- DOI: 10.13009/EUCASS2017-100 - A comparative study of mathematical modeling methods for rocket aerodynamic data
- DOI: 10.13009/EUCASS2017-91 - Comparison of a Closed-Loop Control by Means of High-Fidelity and Low-Fidelity Coupled CFD/RBD Computations
- DOI: 10.13009/EUCASS2017-550 - PITCHING AERODYNAMIC DAMPING IN A FREE FALL PHASE: BACKGROUND THEORIES AND NUMERICAL ANALYSES
- DOI: 10.13009/EUCASS2017-376 - Computational Ground Effect Aerodynamics and Airplane Stability Analysis During Take-off and Landing
- DOI: 10.13009/EUCASS2017-179 - Aircraft Dynamics Identification for Optimal Control
FD - Navigation I
- DOI: 10.13009/EUCASS2017-452 - Synthesis of a control system for relative movement of closely spaced satellites
FP - Buffet and Boundary Layer Transition Delay Control I
- DOI: 10.13009/EUCASS2017-325 - Buffet delay on transonic airfoil by tangential jet blowing
- DOI: 10.13009/EUCASS2017-266 - Localized micro-discharges group DBD vortex generators - disturbances source for active transition control
- DOI: 10.13009/EUCASS2017-291 - Buffet suppression by submicrosecond spark discharge
- DOI: 10.13009/EUCASS2017-345 - Transonic buffet control by plasma actuator with spark discharge
- DOI: 10.13009/EUCASS2017-122 - Simple body force model for Dielectric Barrier Discharge plasma actuator
FP - CFD II
- DOI: 10.13009/EUCASS2017-549 - Preliminary Numerical Aerodatabase of VEGA C Launcher
- DOI: 10.13009/EUCASS2017-582 - Delayed Detached Eddy simulation of separated flows in a planar nozzle
- DOI: 10.13009/EUCASS2017-604 - Study on k-? shear stress transport model corrections applied to rough wall turbulent hypersonic boundary layers
- DOI: 10.13009/EUCASS2017-610 - DNS of spark-ignition in an anode-cathode configuration: impact of plasma chemical kinetics
- DOI: 10.13009/EUCASS2017-389 - Development of a Supersonic Flow Chemical CO Laser Driven by a Chemical Reaction between Carbon Vapor and Oxygen
FP - Rarefield and Real Gas Flows II
- DOI: 10.13009/EUCASS2017-222 - Multi-temperature models for shock heated flows of CO2/CO/O mixture
- DOI: 10.13009/EUCASS2017-230 - Navier-Stokes computation of high-enthalpy non-equilibrium flows with dissociation, vibrational relaxation and ionization
- DOI: 10.13009/EUCASS2017-281 - Numerical simulation of flow over space vehicle in Martian atmosphere
- DOI: 10.13009/EUCASS2017-601 - Modeling, numerical method and validation for the simulation of hypersonic rarefied gas flows
FP - Wind Tunnel and Measurement Techniques II
- DOI: 10.13009/EUCASS2017-213 - Supersonic Wind Tunnel Tests of a Standard Model at High Angles of Attack
- DOI: 10.13009/EUCASS2017-368 - Effect of geometry on the downstream flow topology of a micro ramp in a supersonic turbulent boundary layer: an experimental study
PP - Gel propellants
- DOI: 10.13009/EUCASS2017-253 - Overview on the German Gel Propulsion Technology Activities: Status 2017 and Outlook
- DOI: 10.13009/EUCASS2017-250 - Realization and Run-In of a Gel Combustion Chamber with Optical Access
- DOI: 10.13009/EUCASS2017-268 - Numerical Simulation of a Boron Loaded Gel Fuel Ramjet Combustor
- DOI: 10.13009/EUCASS2017-154 - Green Gelled Propellant Throtteable Rocket Motors for Affordable and Safe Micro-Launchers
- DOI: 10.13009/EUCASS2017-158 - Scalability of Gelled Propellant Rocket Motors
- DOI: 10.13009/EUCASS2017-216 - Design and Realization of a Test Stand for Optical Fluid Dynamic Research of Gels
PP - Hybrid propulsion prototypes
- DOI: 10.13009/EUCASS2017-645 - ZEpHyR - ZARM Experimental Hybrid Rocket: Results of the Propulsion System Tests and Flight of a Small LOX/Paraffin Powered Sounding Rocket
- DOI: 10.13009/EUCASS2017-334 - Development of a 10 kN LOX/HTPB Hybrid Rocket Engine through Successive Development and Testing of Scaled Prototypes
- DOI: 10.13009/EUCASS2017-410 - Getting Ready for Space: Nammo's Development of a 30 kN Hybrid Rocket Based Technology Demonstrator
- DOI: 10.13009/EUCASS2017-468 - QUASI-STEADY AND FORCED TRANSIENT BURNING IN A VORTEX FLOW HYBRID MOTOR
- DOI: 10.13009/EUCASS2017-613 - Thermal Analysis of a Hybrid Rocket Propulsion System for Interplanetary CubeSats
- DOI: 10.13009/EUCASS2017-659 - Liquid booster engine related TMF panel tests
PP - LRE ignition
- DOI: 10.13009/EUCASS2017-49 - Laser ignition of a multi-injector research combustion chamber under high altitude conditions
- DOI: 10.13009/EUCASS2017-336 - Experimental investigation of the ignition, flame propagation and flashback behavior of a premixed green propellant consisting of N2O and C2H4
- DOI: 10.13009/EUCASS2017-674 - Detailed properties of iron oxide solid propellant catalyst
- DOI: 10.13009/EUCASS2017-105 - Formation of solid residues in combustion of boron-containing solid propellants
- DOI: 10.13009/EUCASS2017-324 - Experimental Study on Combustion Process of NEPE Propellant
- DOI: 10.13009/EUCASS2017-544 - Effects of TKX-50 on the properties of HTPB-based composite solid propellant
- DOI: 10.13009/EUCASS2017-98 - Microwave resonator method for measuring transient mass gasification rate of condensed systems
PP - Supersonic combustion and scramjets I
- DOI: 10.13009/EUCASS2017-31 - Thermodynamic performance analysis of scramjet at wide working condition
- DOI: 10.13009/EUCASS2017-218 - Studies on Three-Dimensional Intake with Bleed at M=3.5
- DOI: 10.13009/EUCASS2017-235 - EXPERIMENTS ON FLOW INTERACTION IN A TRANSPIRATION COOLED MODEL SCRAMJET
- DOI: 10.13009/EUCASS2017-459 - Experimental study of the efficiency of the working process in the combustion chamber of the poster module of high-speed civil aircraft HEXAFLY-INT
SI - Space Debris Modeling & Mitigation
- DOI: 10.13009/EUCASS2017-540 - Examination of Spacecraft Anomalies Provides Insight into Complex Space Environment
- DOI: 10.13009/EUCASS2017-519 - Dynamical evolution of space debris in vicinity of GNSS regions
- DOI: 10.13009/EUCASS2017-443 - Sensitivity Analysis for a Space Debris Environment Model
- DOI: 10.13009/EUCASS2017-48 - Dimensional and Scale Analysis Applied to the Preliminary Assessment of the Environment Criticality of Large Constellations in LEO
- DOI: 10.13009/EUCASS2017-335 - SATELLITE DESIGN FOR DEMISE: Thermal Characterisation in Early Re-entry for Dismantlement Mechanisms
- DOI: 10.13009/EUCASS2017-510 - SRM Plume: a candidate as space debris braking system for Just-In-Time Collision Avoidance Maneuver
SI - Unmanned Aerial Vehicules Systems
- DOI: 10.13009/EUCASS2017-184 - Multi Objective Morphing Wing Optimization for an Unmanned Air Vehicle
- DOI: 10.13009/EUCASS2017-89 - Low Level RPAS Traffic Identification and Management
- DOI: 10.13009/EUCASS2017-200 - Conceptual Design of a Hybrid (Turbofan/Solar) Powered HALE UAV
- DOI: 10.13009/EUCASS2017-382 - FlyWin, a H2-lifting gas airship demonstrator
SM - Advanced Materials/Technologies II
- DOI: 10.13009/EUCASS2017-306 - Design and Testing of Liquid Propellant Injectors for Additive Manufacturing
- DOI: 10.13009/EUCASS2017-455 - Additive Layer Manufacturing Technology In Avio Injector Head Design
FD - Avionics and Software
- DOI: 10.13009/EUCASS2017-70 - Reliable High Data RateWireless Sensor Network for Heavy-Lift Launch Vehicles
- DOI: 10.13009/EUCASS2017-489 - FEES: a 1/3U Cubesat Mission for In-Orbit Technology Validation
- DOI: 10.13009/EUCASS2017-232 - Beacon Advertising in an IEEE 802.15.4e TSCH Network for Space Launch Vehicles
- DOI: 10.13009/EUCASS2017-677 - MULTI-GIGABIT PHOTONIC TRANSCEIVERS FOR SPACEFIBRE DATA NETWORKS
- DOI: 10.13009/EUCASS2017-316 - Routes Generation in On-board Space Data Systems with SpaceWire Networks
- DOI: 10.13009/EUCASS2017-399 - Programming technology for autonomous adaptive control using on-board many-core platforms
FD - Control of Aircrafts
- DOI: 10.13009/EUCASS2017-204 - Flight Control Laws Carefree Handling Clearance of a Highly Manoeuvrable Aircraft using Multi-Strategy Adaptive Global Optimization
- DOI: 10.13009/EUCASS2017-402 - Bifucation analysis of the flight dynamics of a fighter aircraft
- DOI: 10.13009/EUCASS2017-202 - WIG-craft flight control concept for the waved sea
- DOI: 10.13009/EUCASS2017-312 - Estimation of Regions of Attraction of Spin Modes
- DOI: 10.13009/EUCASS2017-192 - Robust Control Augmentation System for Flight Envelope Protection Using Backstepping Control Scheme
- DOI: 10.13009/EUCASS2017-228 - HIGH ANGLE OF ATTACK MANEUVERING CONTROL OF F-16 AIRCRAFT BASED ON NONLINEAR DYNAMIC INVERSION AND EIGENSTRUCTURE ASSIGNMENT
FP - Buffet and Boundary Layer Transition Delay Control II and Round Table
- DOI: 10.13009/EUCASS2017-61 - Laminar buffet and flow control
- DOI: 10.13009/EUCASS2017-350 - Effective Plasma Buffet and Drag Control for Laminar Transonic Aerofoil
- DOI: 10.13009/EUCASS2017-341 - Stabilization of Crossflow Instability with Plasma Actuators: Linearized Navier Stokes Simulations
- DOI: 10.13009/EUCASS2017-465 - Direct numerical simulations of transition control in a swept-wing boundary layer using ring-type plasma actuators
FP - Flow Control I
- DOI: 10.13009/EUCASS2017-13 - On volumetric force distribution generated by dielectric barrier discharge actuator
- DOI: 10.13009/EUCASS2017-85 - Control of Plasma and Joule Heating Effects on Supersonic Flow past a Cylindrically Blunted Plate
- DOI: 10.13009/EUCASS2017-114 - Control of Incident Shock Induced Separation at Mach 3.5 using an Array of Steady Micro-Jet Actuators
- DOI: 10.13009/EUCASS2017-270 - Damping of the low veloclity streak by adaptive plasma actuator
- DOI: 10.13009/EUCASS2017-285 - Mitigation of Reflected Shock Wave by Streamwise Plasma Array
- DOI: 10.13009/EUCASS2017-308 - Using of wavy morphing wing for flow and flight control
FP - Rarefield and Real Gas Flows III
- DOI: 10.13009/EUCASS2017-449 - Reducing spacecraft drag in Very Low Earth Orbit through shape optimisation
- DOI: 10.13009/EUCASS2017-470 - Simulation of Unstable Rarefied Gas Flows in Channels and Nozzles for Large Knudsen Numbers
- DOI: 10.13009/EUCASS2017-475 - Scattering of Rarefied Gas Atoms from Poly-Gaussian Rough Surface
FP - Wing Aerodynamics
- DOI: 10.13009/EUCASS2017-103 - V-shaped Wings In Supersonic Flow
- DOI: 10.13009/EUCASS2017-480 - Effects of Wing Flexibility on the Drag of Regional Aviation Aircraft
- DOI: 10.13009/EUCASS2017-653 - Comparison of Turbulence Models Effectiveness for a Delta Wing at Low Reynolds Numbers
PP - Hybrid propulsion fuels I
- DOI: 10.13009/EUCASS2017-107 - Experimental Investigation of the Hydrogen Peroxide - Solid Hydrocarbon Hypergolic Ignition
- DOI: 10.13009/EUCASS2017-473 - Novel, High-Regression Rate Fuels For Hybrid Rocket Motors
- DOI: 10.13009/EUCASS2017-245 - Characterization of HTPB-Based Fuels Containing Multi- Wall Carbon Nanoturbes for Hybrid Propellant
PP - LRE modeling
- DOI: 10.13009/EUCASS2017-18 - Skeletal Kinetic Mechanism of Methane Oxidation for High Pressures and Temperatures
- DOI: 10.13009/EUCASS2017-397 - Numerical study on combustion dynamics of kerosene/GOx under supercritical condition
PP - Nozzles and plumes II
- DOI: 10.13009/EUCASS2017-434 - Ionized Solid Propellant Rocket Exhaust Plume: MiLES Simulation and Comparison to Experiment
- DOI: 10.13009/EUCASS2017-21 - Radio frequency attenuation by a rocket plume using diffraction theory and finite element modeling
- DOI: 10.13009/EUCASS2017-441 - Numerical simulation of radiation in high altitude solid propellant rocket plumes
- DOI: 10.13009/EUCASS2017-579 - Experimental Study of the Infrared Signature Characteristic of a Small Turbojet Engine
PP - Solid propulsion modeling
- DOI: 10.13009/EUCASS2017-144 - A model for solid propellant burning fluctuations using mesoscale simulations
- DOI: 10.13009/EUCASS2017-148 - A numerical mesoscale model for aluminum agglomeration in solid propellants
- DOI: 10.13009/EUCASS2017-430 - CFD Study of Vorticity Patterns and Sound Generation in Simplified Aft-Finocyl Geometries
- DOI: 10.13009/EUCASS2017-432 - Vortex-Sound Modelling in Aft-Finocyl Solid Rocket Motors
- DOI: 10.13009/EUCASS2017-646 - Prediction of the residual thrust of 2nd and 3rd Vega Launcher Solid Rocket Motor stages after the burn-out, due to internal thermal protection pyrolysis
- DOI: 10.13009/EUCASS2017-174 - Computational study of aluminum droplet combustion in different atmospheres
PP - Supersonic combustion and scramjets II
- DOI: 10.13009/EUCASS2017-124 - Experimental investigation of plasma-assisted supersonic combustion
- DOI: 10.13009/EUCASS2017-171 - Numerical Simulation of a Rotating Detonation under Conditions of Premixed and Separate Injection of H2 - O2
- DOI: 10.13009/EUCASS2017-509 - Visualization of conventional and combusting subsonic jet instabilities
SI - Aircraft System Safety
- DOI: 10.13009/EUCASS2017-275 - CARRIER DECK LAUNCHING OF ADAPTED LAND-BASED AIRPLANES
- DOI: 10.13009/EUCASS2017-558 - Research on the Aviation Accident Importance Analysis Based on the Bow-tie model
- DOI: 10.13009/EUCASS2017-276 - Strengths and Weaknesses of the Emergency Evacuation Trial for Transport Airplane Certification
- DOI: 10.13009/EUCASS2017-303 - 6-DOF simulation and the vulnerable area of the Air-to-Air missile to develop an End-game simulator
- DOI: 10.13009/EUCASS2017-562 - PERSONAL OVERHEAD STOWAGE BINS TO EASE FLIGHT BOARDING AND DISEMBARKING AND ENHANCE PASSENGER EXPERIENCE
SI - Space Situational Awarness and Active Debris Removal
- DOI: 10.13009/EUCASS2017-553 - SPOOK - A COMPREHENSIVE SPACE SURVEILLANCE AND TRACKING ANALYSIS TOOL
- DOI: 10.13009/EUCASS2017-678 - Systematic space debris collection using Cubesat constellation
- DOI: 10.13009/EUCASS2017-102 - XXI Century Tower: Laser Orbital Debris Removal and Collision Avoidance
SM - Advanced Materials/Technologies III
- DOI: 10.13009/EUCASS2017-28 - Development of Ultra-Light Weight Carbon Fibre Space Reflector Antenna's Manufacturing Process
- DOI: 10.13009/EUCASS2017-310 - Curing kinetics analysis of carbon/epoxy prepreg for solid rocket motor casings application
- DOI: 10.13009/EUCASS2017-311 - Optimization of curing process of carbon/epoxy prepreg for large Solid Rocket Motor casing
FD - Navigation II
- DOI: 10.13009/EUCASS2017-660 - Advances in the Development of the Attitude Determination and Control System of the CubeSat MOVE-II
- DOI: 10.13009/EUCASS2017-607 - On-board DA-based state estimation algorithm for spacecraft relative navigation
- DOI: 10.13009/EUCASS2017-15 - Integrated SVD/EKF for Nano-satellite Attitude Determination In The Case Of Magnetometer Faults
FD - Simulation and Validation
- DOI: 10.13009/EUCASS2017-259 - Analysis of aircraft trajectory uncertainty using Ensemble Weather Forecasts
- DOI: 10.13009/EUCASS2017-539 - The IXV program FES: MIL and SIL simulation environment for GNC design, development and verification
- DOI: 10.13009/EUCASS2017-162 - A flexible real-time simulation platform dedicated to embedded rocket engine control systems development and testing
- DOI: 10.13009/EUCASS2017-263 - Sector Demand Analysis under Meteorological Uncertainty
- DOI: 10.13009/EUCASS2017-205 - Features of the nanosatellite dynamics in the gravitational and magnetic field of the Earth
FP - Aeroacoustics I
- DOI: 10.13009/EUCASS2017-212 - Numerical Analysis of Acoustic Loads Generated by Supersonic Jets
- DOI: 10.13009/EUCASS2017-568 - Comparison of Two Different CAA Methods for the Prediction of Far-Field Noise from Heated and Unheated Jets
- DOI: 10.13009/EUCASS2017-439 - Helicopter noise simulation and experimental technique for its validation
- DOI: 10.13009/EUCASS2017-638 - Creating a database of helicopter main rotor acoustics for validation of CFD methods
FP - CFD III
- DOI: 10.13009/EUCASS2017-652 - Fluid-kinetic coupling of the BGK and lattice Boltzmann equations
FP - Flow Control II
- DOI: 10.13009/EUCASS2017-351 - Effect of Blowing/Suction through Porous Surface at Supersonic Mach Number
- DOI: 10.13009/EUCASS2017-670 - High speed flow control with nanosecond discharge
- DOI: 10.13009/EUCASS2017-117 - Investigation of Flow Separation Control with Dielectric Barrier Discharge Plasma Actuator
- DOI: 10.13009/EUCASS2017-405 - Flow Control Mechanisms of the Karman-Vortex Generator in Conical Diffuser Separation
FP - Shock Interaction
- DOI: 10.13009/EUCASS2017-63 - The shock-waves interference in the flow around a cylinder mounted on a blunted plate
- DOI: 10.13009/EUCASS2017-84 - Control of Triple-Shock Configurations in High Speed Flows past AD Bodies in Different Gases
- DOI: 10.13009/EUCASS2017-65 - Numerical Simulation of Shock Wave/Laminar Boundary Layer Interaction Over a Blunt Geometry
- DOI: 10.13009/EUCASS2017-97 - Effect of Vibrational Temperature Boundary Condition of Isothermal Wall on Hypersonic Shock Wave Laminar Boundary Layer Interaction of a Hollow Cylinder Flare
PP - Hybrid propulsion fuels II
- DOI: 10.13009/EUCASS2017-251 - Hybrid Rocket Studies Using HTPB/Paraffin Fuel Blends in Gaseous Oxygen Flow
- DOI: 10.13009/EUCASS2017-214 - The Effects of Mechanical Modification Additives on the Regression Rate of Paraffin-Based Fuels for Hybrid Rocket
- DOI: 10.13009/EUCASS2017-596 - Self-disintegration Effects on the Regression Rate of Composite Polymer Particle Paraffin Fuel (CM3PF)
- DOI: 10.13009/EUCASS2017-491 - Imaging Analysis of Boundary-layer Combustion with Tangential and Radial Oxidizer Injection in a Cylinder
PP - Injection and Sprays
- DOI: 10.13009/EUCASS2017-466 - Analyse of the Atomization Process Using Computational Fluid Dynamics
- DOI: 10.13009/EUCASS2017-574 - Including real fuel chemistry in Large-Eddy Simulations
- DOI: 10.13009/EUCASS2017-79 - Visualization coupled with Phase Doppler Interferometry for investigation of cryogenic LOX/nitrogen and LOX/helium sprays
- DOI: 10.13009/EUCASS2017-536 - A Study of Primary Atomization in High-Pressure Fuel Injectors by a Dynamic VOF Solver in OpenFOAM
- DOI: 10.13009/EUCASS2017-147 - Diffuse interface modelling for the primary atomization in cryogenic rocket engines
- DOI: 10.13009/EUCASS2017-691 - Numerical study of acoustic radiation effects on air-assisted jets
PP - Methane rocket engines I
- DOI: 10.13009/EUCASS2017-88 - Effect of Pintle Injector Element Geometry on Combustion in a Liquid Oxygen/Liquid Methane Rocket Engine
- DOI: 10.13009/EUCASS2017-332 - Basic Analysis of a LOX/Methane Expander Bleed Engine
- DOI: 10.13009/EUCASS2017-484 - Architecture Trade-Off for the VEGA-E upper stage LOX/CH4 engine
- DOI: 10.13009/EUCASS2017-483 - Firing Test and Program Progress of the SMSP regenerative combustion chamber
- DOI: 10.13009/EUCASS2017-381 - Subscale Firing Test for Regenerative Cooling LOX/Methane Rocket Engine
- DOI: 10.13009/EUCASS2017-490 - Research and Development Result of Cryogenic Propellant Valve for Small Thrust LOX/methane Rocket Engine
PP - Solid propulsion aluminized propellants
- DOI: 10.13009/EUCASS2017-43 - Smoke oxide particles formation at the burning surface of condensed systems
- DOI: 10.13009/EUCASS2017-532 - Aluminium droplets combustion and SRM instabilities
- DOI: 10.13009/EUCASS2017-469 - AGEING EFFECTS ON NANO-SIZED ALUMINUM REACTIVITY
- DOI: 10.13009/EUCASS2017-327 - Experimental analysis of solid-propellant surface during combustion with shadowgraphy images: new tools to assist aluminum-agglomeration modelling
- DOI: 10.13009/EUCASS2017-585 - Burning Rates of Viton-Coated Aluminum and Water Mixtures
PP - Supersonic combustion and scramjets III
- DOI: 10.13009/EUCASS2017-278 - Complex numerical-experimental investigations of combustion in model high-speed combustor ducts
- DOI: 10.13009/EUCASS2017-106 - Numerical simulation of solid-fuel ramjet combustor with a flame holder
- DOI: 10.13009/EUCASS2017-454 - COMPUTATIONAL RESEARCH OF OPERATION PROCESS IN THE COMBUSTION CHAMBER OF HEXAFLY-INT MODEL IN WIDE RANGE OF FREE STREAM CONDITIONS AND EQUIVALENCE RATIOS
- DOI: 10.13009/EUCASS2017-92 - Validation and further development of 2.5D approach to description of flows in engine ducts
SI - Space System MDO
- DOI: 10.13009/EUCASS2017-575 - ALTAIR - Design & Progress on the Space Launch Vehicle Design
- DOI: 10.13009/EUCASS2017-413 - Multi-Disciplinary Optimisation of Re-entry Vehicles from TAEM to Landing
- DOI: 10.13009/EUCASS2017-650 - Analytical constellation design and link budget computation tool for EO missions
- DOI: 10.13009/EUCASS2017-391 - erformance Evaluation of Altering-intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Using Multi-Disciplinary Optimization
- DOI: 10.13009/EUCASS2017-75 - Overview on the National Programme to Enhance Cryogenic Upper Stage Technologies to Extend European and German Competences in Future Launcher Developments - PROCEED
- DOI: 10.13009/EUCASS2017-223 - New Strategy to Preliminary Design Space Launch Vehicle Based on a Dedicated MDO Platform
SM - Structural Dynamics I
- DOI: 10.13009/EUCASS2017-206 - Simulation of Fluid Structure Interaction in Overexpanded Cold Gas Rocket Nozzles using the DLR TAU Code
- DOI: 10.13009/EUCASS2017-299 - Hypersonic Fluid-Structure Interaction on a Cantilevered Plate
- DOI: 10.13009/EUCASS2017-38 - Experimental characterization of the acoustics of the future Ariane 6 launch pad
- DOI: 10.13009/EUCASS2017-80 - Design optimization and test campaign of a 1/50th ARIANE 5 representative dynamic model subjected to blast waves
- DOI: 10.13009/EUCASS2017-634 - Dynamic aeroelastic simulation of composite wing for HALE UAV application
- DOI: 10.13009/EUCASS2017-90 - Nonlinear flutter analysis with uncertainties based on Describing Function and Structured Singular Value with an IQC validation
FD - FDIR and Control
- DOI: 10.13009/EUCASS2017-692 - Turning model-based FDIR theory into practice for aerospace and flight-critical systems
- DOI: 10.13009/EUCASS2017-51 - A multi-objective Hinfinity design framewok for helicopter PID control tuning with handling qualities requirements
- DOI: 10.13009/EUCASS2017-556 - FDI Design and Verification using a High-Fidelity Industrial Airbus Nonlinear Simulator
- DOI: 10.13009/EUCASS2017-195 - Neural Network-Based Nonlinear Dynamic Inversion Control of Variable-Span Morphing Aircraft
- DOI: 10.13009/EUCASS2017-321 - Reconfiguration control method for non-redundant actuator faults on UAV
- DOI: 10.13009/EUCASS2017-62 - Fault Tolerant Integrated Barometric-Inertial-GPS Altimeter
FD - Orbit control
- DOI: 10.13009/EUCASS2017-50 - Solving the Minimum-Fuel Low-Thrust Geostationary Station Keeping Problem via the Switching Systems Theory
- DOI: 10.13009/EUCASS2017-151 - Optimal bi-impulse orbital transfer between coplanar orbits
- DOI: 10.13009/EUCASS2017-289 - Fast Aerodynamic Establishment of a Constellation of CubeSats
- DOI: 10.13009/EUCASS2017-39 - Formation Flying Along Halo Orbit Using Switching Hamiltonian Structure Preserving Control
FP - Boundary Layer Transition I
- DOI: 10.13009/EUCASS2017-60 - BiGlobal stability analysis of the wake behind an isolated roughness element in hypersonic flow
- DOI: 10.13009/EUCASS2017-120 - TRANSITION REVERSAL ON BLUNT OGIVE BODY OF REVOLUTION AT HYPERSONICSPEEDS
- DOI: 10.13009/EUCASS2017-128 - Problems with discontinuous boundary conditions describing laminar flows at high Reynolds numbers
- DOI: 10.13009/EUCASS2017-161 - The investigation of laminar-turbulent transition behind the localized roughness on the swept wing in the favorable pressure gradient region
- DOI: 10.13009/EUCASS2017-163 - The influence of two-dimensional roughness element on boundary flow structure in the favorable pressure gradient region of the swept wing
- DOI: 10.13009/EUCASS2017-682 - Forward-Facing Steps Induced Transition in a Subsonic Boundary Layer
FP - International Workshop on ICING I
- DOI: 10.13009/EUCASS2017-668 - Icephobic Performance of Superhydrophobic Coatings: A Numerical Analysis
- DOI: 10.13009/EUCASS2017-482 - Prediction of rivulet transition in anti-icing applications
- DOI: 10.13009/EUCASS2017-153 - Experimental Study of Unsteady Aerodynamic Characteristics of Transport Aircraft in Icing Conditions
- DOI: 10.13009/EUCASS2017-687 - An Integrated Approach to Swept Wing Icing Simulation
- DOI: 10.13009/EUCASS2017-625 - Comparison of extensional and flexural modes for the design of piezoelectric ice protection systems
FP - Separated Flows and Shear Layers
- DOI: 10.13009/EUCASS2017-82 - New type of singularity in the near-wall region of 3D boundary layer over the runoff plane and the flow structure in its vicinity
- DOI: 10.13009/EUCASS2017-86 - DYNAMIC LAYER FORMATION IN THE REATTACHMENT ZONE FOR A SUPERSONIC LAMINAR SEPARATION FLOW
- DOI: 10.13009/EUCASS2017-183 - Mechanism of ideal gas separation for bodies in a supersonic flow
- DOI: 10.13009/EUCASS2017-619 - On the Structure of Large Scale Separations in Hypersonic Flows
- DOI: 10.13009/EUCASS2017-672 - Mathematical model for LES of evolution of far vortex wake behind an airplane
PP - Air Breathing I
- DOI: 10.13009/EUCASS2017-371 - Hybrid LES-RANS simulations of enthalpy reduction in T-shape chamber by means of transverse cold air injection
- DOI: 10.13009/EUCASS2017-17 - Air Breathing Engine Theory at the Space Thermostat Presence
- DOI: 10.13009/EUCASS2017-55 - Preliminary Investigation on the Starting Characteristics and Flow Control of an Inward-turning Inlet
PP - Green solid propellants GRAIL Workshop
- DOI: 10.13009/EUCASS2017-560 - GRAIL: Green Solid Propellants for Launchers
- DOI: 10.13009/EUCASS2017-502 - Calculated and experimental binary phase diagrams for ADN and AN based solid propellants - H2020 GRAIL project
- DOI: 10.13009/EUCASS2017-429 - Burning Behavior of ADN-Based Propellants Loaded with Al-Mg Mechanically Activated Powders
- DOI: 10.13009/EUCASS2017-478 - Synthesis, characterization and treatment of alane (aluminium hydride, AlH3)
- DOI: 10.13009/EUCASS2017-520 - Catalyst screening for ammonium nitrate oxidizer
- DOI: 10.13009/EUCASS2017-72 - Burning Behavior of Aluminized ADN/PSAN Propellants
PP - Hybrid propulsion numerical modeling I
- DOI: 10.13009/EUCASS2017-506 - Numerical Analysis of Turbulent Combustion in Hybrid Rocket Motor with Swirling and Axial Oxidizer Injection
- DOI: 10.13009/EUCASS2017-157 - Development of an Eddy Dissipation Model for the use in Numerical Hybrid Rocket Engine Combustion Simulation
- DOI: 10.13009/EUCASS2017-611 - Combined fluid-dynamic modelling of hybrid rocket internal ballistics and nozzle heat transfer
- DOI: 10.13009/EUCASS2017-477 - Numerical Simulation of Vortex Combustion in a Hybrid Rocket Motor
PP - Methane rocket engines II
- DOI: 10.13009/EUCASS2017-552 - Highly reusable Lox/LCH4 ACE rocket engine designed for SpacePlane: Technical Maturation progress via key system demonstrators results
- DOI: 10.13009/EUCASS2017-537 - Prometheus, a LOX/LCH4 reusable rocket engine
- DOI: 10.13009/EUCASS2017-370 - Utilization of LOx/LCH4 Expander-Bleed Cycles for Upper Stage Engine Applications
- DOI: 10.13009/EUCASS2017-360 - The HYPROB LOX-LCH4 Demonstrator: status of the manufacturing and experimental activities
- DOI: 10.13009/EUCASS2017-577 - Multi Purposes Reusable Lox/CH4 Bleed Rocket Engine
- DOI: 10.13009/EUCASS2017-583 - Test of flow deflector demonstrators in LOX/Methane combustion gases
PP - Propellant management and tanks
- DOI: 10.13009/EUCASS2017-146 - Liquid hydrogen low Bond number reorientation: Experiment and numeric comparison
- DOI: 10.13009/EUCASS2017-471 - Multi-body modeling for fluid sloshing dynamics investigation in fast spinning rockets
- DOI: 10.13009/EUCASS2017-511 - Active Slosh Control and Damping - Simulation and Experiment
- DOI: 10.13009/EUCASS2017-115 - Enhancement of fuel evaporation in microgravity conditions under the effect of ultrasound techniques
- DOI: 10.13009/EUCASS2017-220 - Pressurization system for a cryogenic propellant tank in a pressure-fed high-altitude rocket
- DOI: 10.13009/EUCASS2017-367 - Development and verification of an oxygen mass-flow regulator under high temperature and pressure conditions
- DOI: 10.13009/EUCASS2017-59 - TRL 5 Tests of a Sub-Scale LH2 Feed Line Evaporation Cooler
PP - Propulsion Systems
- DOI: 10.13009/EUCASS2017-626 - Possibility of using thermal decomposition of hydrogen peroxide for low thrust propulsion system application
- DOI: 10.13009/EUCASS2017-573 - Antigravity based propulsion systems - a new era in astronautics and aeronautics
- DOI: 10.13009/EUCASS2017-701 - Modeling and validation of propulsion system for small battery powered electric aircraft
SI - Space Systems Concepts
- DOI: 10.13009/EUCASS2017-592 - CHEOPS First ESA Small Scientific Mission
- DOI: 10.13009/EUCASS2017-680 - CALLISTO PROJECT - REUSABLE FIRST STAGE ROCKET DEMONSTRATOR
- DOI: 10.13009/EUCASS2017-57 - Ariane 6 launcher requirements for solid rocket motor
- DOI: 10.13009/EUCASS2017-624 - Conceptual Design of the Descent Subsystem for the Safe Atmospheric Re-Entry Flight of Space Rider
- DOI: 10.13009/EUCASS2017-563 - RECOVERY OF SOUNDING ROCKETS USING RETRACTABLE WINGS FOR CONTROLLED DESCEND
- DOI: 10.13009/EUCASS2017-497 - On the use of the concept of Equivalent Single Stage Launcher
- DOI: 10.13009/EUCASS2017-273 - Photonic swarm for low frequency radio astronomy in Space
SM - Structural Dynamics II
- DOI: 10.13009/EUCASS2017-29 - Automatic estimation of modal parameters using a hybrid method of MOPSO and k-means clustering in the time-frequency domain
- DOI: 10.13009/EUCASS2017-337 - Dynamic similarity of large 3D frame structures
- DOI: 10.13009/EUCASS2017-121 - INVESTIGATION OF BALL JOINTS UNDER STATIC AND DYNAMIC LOADS
- DOI: 10.13009/EUCASS2017-176 - A hybrid FE-SEA model reduction method to obtain detailed responses at chosen locations from a large launch vehicle model
- DOI: 10.13009/EUCASS2017-34 - Benchmark and Application of Operational Modal Analysis Techniques on Ariane 5 Flight Records
- DOI: 10.13009/EUCASS2017-358 - Vibration Reduction in a Helicopter Using Active Twist Rotor Blade Method
FD - Control/Guidance of Launchers and Spacecrafts
- DOI: 10.13009/EUCASS2017-257 - Structured H-infinity and Linear Parameter Varying Control Design for the VEGA Launch Vehicle
- DOI: 10.13009/EUCASS2017-597 - Design of MICROSCOPE's Attitude-Guidance Strategy for Star-Tracker's Moon-Glare Management
- DOI: 10.13009/EUCASS2017-152 - A Systematic Performance-oriented Tuning for Space Exploration Descent & Landing Guidance
- DOI: 10.13009/EUCASS2017-664 - Magnetic Attitude Control for the MOVE-II Mission
- DOI: 10.13009/EUCASS2017-435 - Autonomous GNC/IP for Approach and Hovering of irregular small bodies
- DOI: 10.13009/EUCASS2017-530 - Optimal Control of Spacecraft Using Electrostatic forces
FP - Boundary Layer Transition II
- DOI: 10.13009/EUCASS2017-210 - Evolution of perturbations of laminar flow behind the ledge of the surface generated by its localized vibration
- DOI: 10.13009/EUCASS2017-211 - Generation of disturbances by vibrations of localized surface in a flat plate boundary layer
- DOI: 10.13009/EUCASS2017-288 - Parabolized stability analysis of chemically reacting boundary layer flows in equilibrium conditions
- DOI: 10.13009/EUCASS2017-292 - On the origin and development of the streaks in flat plate supersonic boundary layer
- DOI: 10.13009/EUCASS2017-295 - The influence of small angle of attack on disturbances evolution and transition to turbulence in supersonic boundary layer on swept wing
FP - Computational and Experimental Aerodynamics of Air Vehicules I
- DOI: 10.13009/EUCASS2017-95 - AERODYNAMIC SHAPES OPTIMIZATION ON THE BASE OF METHOD OF LOCAL LINEARIZATION
- DOI: 10.13009/EUCASS2017-119 - PCA-Assisted Local Flow Field Analysis and its Application in Aerodynamic Optimization
- DOI: 10.13009/EUCASS2017-194 - Numerical Research of A Propeller Plane Based on Actuator Disc Model
- DOI: 10.13009/EUCASS2017-255 - Numerical simulation of the flow around a flapping-wing micro air vehicle in free flight
- DOI: 10.13009/EUCASS2017-261 - Preliminary Design and Performance Verification of a Guided Entry Thruster System for Precision Landing on Mars
- DOI: 10.13009/EUCASS2017-283 - Aerodynamic peculiarities of 3D supersonic flow over space vehicle
FP - International Workshop on ICING II
- DOI: 10.13009/EUCASS2017-555 - Ice Accretion Roughness Measurements and Modeling
- DOI: 10.13009/EUCASS2017-372 - Accounting for wall roughness effects in turbulence models : a wall function approach
- DOI: 10.13009/EUCASS2017-258 - Multi-Layer Icing Methodologies for Conservative Ice Growth
- DOI: 10.13009/EUCASS2017-400 - 3D ice accretion modeling using an integral boundary layer method
- DOI: 10.13009/EUCASS2017-517 - Modeling of the reemitted droplets on a small scale rotating FAN model: comparison between experimental and numerical results
- DOI: 10.13009/EUCASS2017-269 - ICING SIMULATIONS ON ENGINE INTAKE
FP - Launcher Aerodynamics
- DOI: 10.13009/EUCASS2017-116 - Simulation of the reentry vehicle supersonic brake jets interaction with landing surface
- DOI: 10.13009/EUCASS2017-561 - Numerical investigation of the turbulent wake of a generic space launcher at transonic speed
- DOI: 10.13009/EUCASS2017-496 - Towards an efficient and robust numerical strategy for fast aerodynamic performance prediction on launch vehicles
- DOI: 10.13009/EUCASS2017-499 - Comparison of high speed PIV experiments, unsteady pressure measurements and DES computations of a transonic Ariane 5 base-flow using POD
Issues for Future of aerospace
- DOI: 10.13009/EUCASS2017-125 - Experimental Evaluation of the Pollutant and Noise Emissions of the GTCP 36-300 Gas Turbine operated with Kerosene and with a Low NOx Micromix Hydrogen Combustor
- DOI: 10.13009/EUCASS2017-606 - Large Eddy Simulation of trailing edge cutback film cooling: Impact of internal stiffening ribs on the adiabatic effectiveness
- DOI: 10.13009/EUCASS2017-487 - Preliminary Results from a Plasma-Assisted 7-Point LDI Combustor
- DOI: 10.13009/EUCASS2017-249 - Towards a Novel 0D Gas Turbine Combustor Modeling: Bridging the Gap Between Dimensional and Engine Performance Approaches
- DOI: 10.13009/EUCASS2017-586 - The efficiency of usage of new construction rotors with the ability simultaneously change basic geometric parameters in the dynamics and their consumption in the fields of aviation and high-power wind stations
PP - Hybrid propulsion numerical modeling II
- DOI: 10.13009/EUCASS2017-614 - CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats
- DOI: 10.13009/EUCASS2017-616 - Transition of Combustion Instability by Swirl Injector in Hybrid Rocket
- DOI: 10.13009/EUCASS2017-191 - The Oscillation Characteristics of Reactive Flow in the Hybrid Rocket Post Chamber
- DOI: 10.13009/EUCASS2017-629 - Modeling of High Density Polyethylene Regression Rate in the Simulation of Hybrid Rocket Flowfields
PP - LRE II
- DOI: 10.13009/EUCASS2017-140 - Next-Generation RS-25 Engines for the NASA Space Launch System
- DOI: 10.13009/EUCASS2017-69 - Implications of Cycle Variants, Propellant Combinations and Operating Regimes on Fatigue Life Expectancies of Liquid Rocket Engines
- DOI: 10.13009/EUCASS2017-535 - Effects of Cu-alloy Material Properties on Lifetime of a Combustion Chamber with or without a Thermal Barrier Coating
- DOI: 10.13009/EUCASS2017-417 - Promising HMS approaches for liquid rocket engines
- DOI: 10.13009/EUCASS2017-42 - Rocket Propulsion in TAU: An Overview of the DLR ProTAU Project
PP - Turbomachines
- DOI: 10.13009/EUCASS2017-189 - The Modified Fuel Turbopump of 2nd stage engine for H3 launch vehicle
- DOI: 10.13009/EUCASS2017-241 - On the effect of axial turbine rotor blade design on efficiency: a parametric study of the Baljé-diagram
- DOI: 10.13009/EUCASS2017-40 - Analytical and numerical assessment of axial thrust balancing systems in liquid rocket engine LOx turbopumps
SI - Hypersonics Systems
- DOI: 10.13009/EUCASS2017-505 - SpaceLiner Concept as Catalyst for Advanced Hypersonic Vehicles Research
- DOI: 10.13009/EUCASS2017-408 - From MDO to detailed design of Hypersonic Morphing Cabin Escape Systems
- DOI: 10.13009/EUCASS2017-53 - Hypersonic Morphing for the SpaceLiner Cabin Escape System
- DOI: 10.13009/EUCASS2017-35 - A Novel Design Technique of Hypersonic Gliding Vehicle
SM - Structural Modelling. Testing. Validation and Optimization I
- DOI: 10.13009/EUCASS2017-240 - The Influence of Spar Location on the Elastic Deformation and the Weight Estimation of a Swept-back, High Altitude, Solar Powered Flying Wing UAV
- DOI: 10.13009/EUCASS2017-104 - Quieter Propellers
- DOI: 10.13009/EUCASS2017-19 - Modelling Powder Bed Additive Manufacturing Defects
SM - Temperature Resistants Materials/Protections I
- DOI: 10.13009/EUCASS2017-180 - Implementation of Approximate Ablation Model in Aerodynamic Heating Prediction Tool
- DOI: 10.13009/EUCASS2017-262 - Aero-Thermal Post Flight Analysis of IXV Control Surfaces
FD - Flight Control of UAVs
- DOI: 10.13009/EUCASS2017-329 - Wind rejection via quasi-continuous sliding mode technique to control safely a mini drone
- DOI: 10.13009/EUCASS2017-460 - Adaptive augmentation of the attitude control system for a multirotor UAV
- DOI: 10.13009/EUCASS2017-219 - Validation of Natural Frequencies Formulas of Flight Modes for Small UAVs
- DOI: 10.13009/EUCASS2017-472 - Accurate positioning of multirotor UAVs for civil infrastructure monitoring
- DOI: 10.13009/EUCASS2017-169 - Compagnin et al Autoport System a Suite of Sensors and Mechanisms for Mars UAVs
- DOI: 10.13009/EUCASS2017-411 - Experimental validation of Unmanned Aerial Vehicles to tune PID controllers in open source autopilots
FP - Boundary Layer Transition III
- DOI: 10.13009/EUCASS2017-309 - Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layer
- DOI: 10.13009/EUCASS2017-344 - Effect of nose-tip roughness on laminar-turbulent transition
- DOI: 10.13009/EUCASS2017-419 - CFD and Experimental Simulation of the Laminar-Turbulent Transition on the HEXAFLY-INT Glider Model
- DOI: 10.13009/EUCASS2017-578 - Recalibration of the k-omega-gamma Transition Model in UNITs and Application to Transition Prediction of Blunt Cones
- DOI: 10.13009/EUCASS2017-594 - Pressure gradient effects on wake flow instabilities behind isolated roughness elements on re-entry capsules
- DOI: 10.13009/EUCASS2017-656 - Direct Numerical Simulation of Transitional Boundary Layer with Local Separation in Hypersonic Flight
FP - Computational and Experimental Aerodynamics of Air Vehicules III
- DOI: 10.13009/EUCASS2017-365 - Aerodynamic Design on a Martian Micro Air Vehicle
- DOI: 10.13009/EUCASS2017-571 - Longitudinal Stability Measurements of a Winged Biconic Configuration in Supersonic Flow
- DOI: 10.13009/EUCASS2017-318 - Effect of the wing trailing-edge flaps and spoilers position on the jet-vortex wake behind an aircraft during takeoff and landing run
- DOI: 10.13009/EUCASS2017-380 - Drag prediction and decomposition of a real aircraft based on middle-field and far-field methods
FP - Heat Transfer
- DOI: 10.13009/EUCASS2017-30 - Numerical exploration on the drag ad heat flux reduction mechanism of blunted cone with aerodisks
- DOI: 10.13009/EUCASS2017-68 - Numerical modeling of continuous blowing surface in hypersonic boundary layers
- DOI: 10.13009/EUCASS2017-81 - Physical mechanisms of increased heat flux zone appearance and laminar-turbulent transition in the boundary layer on blunted delta wings at high freestream velocities
- DOI: 10.13009/EUCASS2017-495 - Duplication of reacting boundary layer between hypersonic flight and Plasmatron facility
- DOI: 10.13009/EUCASS2017-87 - Modeling of radiative cooling of disperse flows of the low
FP - International Workshop on ICING III
- DOI: 10.13009/EUCASS2017-512 - Physics of SLD Impact and Solidification
- DOI: 10.13009/EUCASS2017-175 - Experimental investigation of SLD impact phenomena
- DOI: 10.13009/EUCASS2017-265 - From high altitude clouds to an icing wind tunnel: en route to understand ice crystal icing
- DOI: 10.13009/EUCASS2017-314 - Experimental and theoretical investigations of solid-phase ice accretion
- DOI: 10.13009/EUCASS2017-339 - In-Flight Mixed Phase Ice Accretion Prediction on Finite Wings with TAICE-3D
PP - Electrical propulsion
- DOI: 10.13009/EUCASS2017-32 - Numerical Model of an Helicon Plasma Source for Space Propulsion Application
- DOI: 10.13009/EUCASS2017-126 - Research of electron distribution function traits in discharge chamber of ion thruster using 'Particle-in-cell' simulation
- DOI: 10.13009/EUCASS2017-138 - The low-current cathode for a small power electric propulsion
- DOI: 10.13009/EUCASS2017-139 - Experimental studies of an ion optic system with improved mechanical strength
- DOI: 10.13009/EUCASS2017-378 - Multiphysics Model Validation of Resistojets with Concentric Tubular Heat Exchanger
PP - GOX/GCH4 combustion
- DOI: 10.13009/EUCASS2017-340 - High-speed and Emission Imaging of a Coaxial Single Element GOX/GCH4 Rocket Combustion Chamber
- DOI: 10.13009/EUCASS2017-366 - Heat flux and temperature evaluation in a rectangular multi-element GOX/GCH4 combustion chamber using an inverse heat conduction method
- DOI: 10.13009/EUCASS2017-605 - Large Eddy Simulation of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor
- DOI: 10.13009/EUCASS2017-173 - Numerical Investigation of a 7-Element GOX/GCH4 Subscale
- DOI: 10.13009/EUCASS2017-242 - Investigation on Recess Variation of a Shear Coax Injector in a GOX-GCH4 Rectangular Combustion Chamber with Optical Access
- DOI: 10.13009/EUCASS2017-347 - Mapping of H2O concentration and temperature in a turbulent methane air diffusion flame using multispectral absorption tomography
PP - Green liquid propellants II
- DOI: 10.13009/EUCASS2017-364 - Green Liquid Oxidisers Basing on Solutions of ADN and AN in Hydrogen Peroxide for Hypergolic Propellants with High Performance
- DOI: 10.13009/EUCASS2017-349 - Performance Comparison between Extruded and Printed Ceramic Monoliths for Catalysts
- DOI: 10.13009/EUCASS2017-45 - Matrix conversion of natural and associated petroleum gases to syngas - new developments and possibilities
PP - Hybrid propulsion experimental investigations
- DOI: 10.13009/EUCASS2017-149 - Experimental and Numerical Evaluation of the Radiative Wall Heat Flux in the Post-Chamber of a Paraffin-Based Hybrid Rocket Engine
- DOI: 10.13009/EUCASS2017-661 - Experimental Evaluation of Pressure-Swirl Injection System over Solid Fuel Regression Rate in Hybrid Rockets
- DOI: 10.13009/EUCASS2017-159 - Optical Analysis of the Liquid Layer Combustion of Paraffin-based Hybrid Rocket Fuels
- DOI: 10.13009/EUCASS2017-133 - Design and experimental Evaluation of Liquid Oxidizer Injection System for Hybrid Rocket Motors
- DOI: 10.13009/EUCASS2017-414 - Development and Test of an Innovative Hybrid Rocket Combustion Chamber
- DOI: 10.13009/EUCASS2017-425 - Development of a Cavitating Pintle for a Throttleable Hybrid Rocket Motor
PP - Thermo-acoustics instabilities
- DOI: 10.13009/EUCASS2017-64 - A numerical analysis of aluminum droplet combustion driven instabilities in solid rocket motors
- DOI: 10.13009/EUCASS2017-172 - Modelling Flame Response of a Co-axial LOx/GH2 Injection Element to High Frequency Acoustic Forcing
- DOI: 10.13009/EUCASS2017-267 - On the effect of acoustic absorbers coupled to rocket combustors
- DOI: 10.13009/EUCASS2017-352 - Large-Eddy Simulations of a sub-scale liquid rocket combustor: influence of fuel injection temperature on thermo-acoustic stability
- DOI: 10.13009/EUCASS2017-461 - Low order investigation on longitudinal combustion instability in a variable geometry single element combustor
SI - Launch of Small Payloads
- DOI: 10.13009/EUCASS2017-346 - Hybrid Sounding Rocket HEROS: TRL 9
- DOI: 10.13009/EUCASS2017-221 - ALTAIR Orbital Module Preliminary Mission and System Design
- DOI: 10.13009/EUCASS2017-679 - Small Payload Transfers from Earth to LEO and LEO to Interplanetary Space using Lasers
- DOI: 10.13009/EUCASS2017-96 - ARES14BI 'Hydra' - a two-stage experimental rocket project within the PERSEUS program
- DOI: 10.13009/EUCASS2017-600 - Small Innovative Launcher for Europe: achievement of the H2020 project SMILE
- DOI: 10.13009/EUCASS2017-286 - Cost Estimating of Commercial Smallsat Launch Vehicles
SI - Reentry Survivability & Space Surveillance
- DOI: 10.13009/EUCASS2017-569 - Upgrade of ESA's Debris Risk Assessment and Mitigation Analysis (DRAMA) Tool: Spacecraft Entry Survival Analysis Module
- DOI: 10.13009/EUCASS2017-603 - Development of New Analytical Models of Pressure and Heat Transfer Distributions on Space Debris during Uncontrolled Atmospheric Entry: Planar Bodies
- DOI: 10.13009/EUCASS2017-599 - DSMC-based Correction Factor for Low-fidelity Hypersonic Aerodynamics of Re-entering Objects and Space Debris
- DOI: 10.13009/EUCASS2017-521 - Monte Carlo analysis of a LEO reentry mission by solid rocket propulsion
- DOI: 10.13009/EUCASS2017-684 - Trushlyakov Research of thermal loading of the separated rocket design elements in the atmospheric phase of the descent trajectory EUCASS2017
SM - Structural Modeling. Testing. Validation and Optimization II
- DOI: 10.13009/EUCASS2017-326 - Dynamical Characterization of Propellant using the DMA
- DOI: 10.13009/EUCASS2017-384 - Probabilistic Approach to Damage Modeling of Aviation Composite Materials
- DOI: 10.13009/EUCASS2017-615 - Modification of Spacecraft Materials under Electron Radiation
- DOI: 10.13009/EUCASS2017-531 - Ground Test for Spacecraft Charging and Discharging at NRIAG-Egypt
- DOI: 10.13009/EUCASS2017-438 - Solar Concentrator Demonstrator for PocketQubes
SM - Temperature Resistants Materials/Protections II
- DOI: 10.13009/EUCASS2017-330 - IXV Thermal Protection System Post-Flight Preliminary analysis
- DOI: 10.13009/EUCASS2017-428 - Development of an Italian Technology for CMC Control Surface for Re-entry Applications
- DOI: 10.13009/EUCASS2017-433 - Investigation of the Thermal Protective Coating for the Experimental Flight Test Vehicle within the International HEXAFLY-INT Project
- DOI: 10.13009/EUCASS2017-504 - STABILIZATION OF C/C BASED SHELL STRUCTURES FOR HIGH TEMPERATURE RE-ENTRY
Posters
- DOI: 10.13009/EUCASS2017-46 - Ignition of high-energy materials containing boron and aluminum diboride
- DOI: 10.13009/EUCASS2017-77 - An Experimental Study on Pressure Loss in Spiral Cooling Channels
- DOI: 10.13009/EUCASS2017-94 - A Study on Missile Autopilot Design using Nonlinear Adaptive Sliding Mode Control Scheme
- DOI: 10.13009/EUCASS2017-190 - AGGLOMERATION AND COMBUSTION COMPLETENESS OF BORON IN COMPOSITE PROPELLANT
- DOI: 10.13009/EUCASS2017-203 - Design and Analysis on the Fire Prevention System for Space Launch Vehicle during the Flight
- DOI: 10.13009/EUCASS2017-233 - Combustion of Sprays from Triplet Injector with Green Propellants: Ethyl Alcohol and Hydrogen Peroxide
- DOI: 10.13009/EUCASS2017-264 - Guidance, Navigation, and Control for Formation Flying Using Differential Drag
- DOI: 10.13009/EUCASS2017-279 - Measurements and numerical simulation of wall heat fluxes in a single-element GO2/GCH4 rocket combustor
- DOI: 10.13009/EUCASS2017-293 - OPTIMIZATION OF THE STARTUP SEQUENCE OF A LIQUID-PROPELLANT ROCKET ENGINE
- DOI: 10.13009/EUCASS2017-301 - Numerical Study of Flow Characteristics of the 14-X B Hypersonic Aerospace Vehicle Inlet with Blunted Leading Edge
- DOI: 10.13009/EUCASS2017-412 - Dusty Plasma Void Dynamics in Unmoving and Moving Flows
- DOI: 10.13009/EUCASS2017-431 - Postbuckling Analyses of Cylindrical Structures using Hybrid-Grid Systems for Derivation of Knockdown factor
- DOI: 10.13009/EUCASS2017-500 - PERSEUS : Composite Nozzle Realization
- DOI: 10.13009/EUCASS2017-526 - Development of a Probe for Particle Collection in High-Temperature, Supersonic Flow: Conceptual and Detailed Design
- DOI: 10.13009/EUCASS2017-546 - Preliminary analysis for the design of a PrandtlPlane transport aircraft
- DOI: 10.13009/EUCASS2017-547 - KAPPA: an object-oriented C++ library for kinetic theory computations
- DOI: 10.13009/EUCASS2017-630 - Design of Inlet Distortion Generators for Direct-Connect Scramjet Combustors
- DOI: 10.13009/EUCASS2017-635 - Thermal analysis and performance of a pressure gain combustion system
- DOI: 10.13009/EUCASS2017-644 - ReFEx: Reusability Flight Experiment - A Flight Experiment to Demonstrate Controlled Aerodynamic Flight from Hypersonic to Subsonic Velocities with a Winged RLV
- DOI: 10.13009/EUCASS2017-654 - EXTERNAL IGNITION DEVICE OR GROUND IGNITION FOR A CRYOGENIC H2/O2 PROPELLANT FED ROCKET ENGINE
- DOI: 10.13009/EUCASS2017-663 - Features of control system of space solar power station
- DOI: 10.13009/EUCASS2017-688 - Space-based Sustainability Management System (S-b SMS) : Bridging the Gap