DOI: 10.13009/EUCASS2022-4495
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Feasibility Study of a Hybrid Business Turboprop
Pedro L?pez-Pernas and Rodrigo Mart?nez-Val* Universidad ...
DOI: 10.13009/EUCASS2022-4496
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
On the matching between design specifications and payload-range efficiency of transport airplanes
Alejandro ...
DOI: 10.13009/EUCASS2022-4507
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Analysis of conjunctions between two satellites with no communication
Romain Lucken? ? and Alexis Petit? ...
DOI: 10.13009/EUCASS2022-4535
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Experimental investigation of the regression rate in an endburning swirling flow hybrid rocket engine
Tomasz ...
DOI: 10.13009/EUCASS2022-4540
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Research and Test Activities on Advanced Rocket Propellants at DLR?s Institute of Space Propulsion in ...
DOI: 10.13009/EUCASS2022-4541
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Loads prediction at early stage of water landing on amphibious aircraft with a V-shaped hull
Yujin Lu1,2, ...
DOI: 10.13009/EUCASS2022-4543
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Preliminary study of the high-frequency instability of an aerospike rocket engine
Federico Rossi*, Roman ...
DOI: 10.13009/EUCASS2022-4549
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Restrike model for an MHD solver: application to plasmaassisted supersonic combustion in scramjet
Bourlet ...
DOI: 10.13009/EUCASS2022-4555
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Adaptative structures:
the key for future airship certification
A challenge for light flexible structure ...
DOI: 10.13009/EUCASS2022-4558
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
E?cient and accurate strategy for high-?delity simulations of solid rocket motor ignition
Laurent Fran?ois ...
DOI: 10.13009/EUCASS2022-4565
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Space grade Biomethane production for Themis reusable stage demonstrator
Michal KURELA* Pascal NOIR* ...
DOI: 10.13009/EUCASS2022-4573
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
REST HF-9 test case: Large-Eddy Simulation of DLR?s BKD configuration
Thomas Schmitt1? , Gabriel Staffelbach2 ...
DOI: 10.13009/EUCASS2022-4583
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Non-linear one-dimensional combustion response model integration in a CFD software, test case and simplified ...
DOI: 10.13009/EUCASS2022-4600
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Sustainable Supersonic Transport: a Case Study on Variable Pitot Inlets
Stefan Kazula, Klaus H?schler ...
DOI: 10.13009/EUCASS2022-4611
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Analysis of the fire reaction of fibre reinforced polymer matrix composites exposed to a flame
Wang X.*, ...
DOI: 10.13009/EUCASS2022-4626
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Description of an Air-Oil Test Set-Up for ACOC Heat Exchangers Testing
Jo?lle Vinck? , Olivier Berten ...
DOI: 10.13009/EUCASS2022-4634
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Wind Tunnel Experiments of the CALLISTO VTVL Launcher in the TMK and HST Wind Tunnels
Johannes Riehmer1, ...
DOI: 10.13009/EUCASS2022-4637
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Numerical Investigation on the Aerodynamic Design of Quadrotor Blades Operating in the Martian Atmosphere
Manuel ...
DOI: 10.13009/EUCASS2022-4643
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Experimental study on the effect of cryogenic two-phase flow inlet conditions on the suction capacity ...
DOI: 10.13009/EUCASS2022-4647
9TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Development of Rocket Engine with Continuously Rotating Detonation supplied by Liquid Propellants
Micha? ...