DOI: 10.13009/EUCASS2025-001
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Wear of aircraft materials in case of emergency landing
situations: an experimental investigation
S. Penaherrera ...
DOI: 10.13009/EUCASS2025-002
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
BLDC-Motor-Driven Multipurpose Control Valve for Liquid
Rocket Engine of KSLV-III
Taekyu Jung*†, Minsung ...
DOI: 10.13009/EUCASS2025-003
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
A 0D Model for Rotating Detonation Engine Propulsive
Performance Estimation
Elouan Maitre* and Bassam ...
DOI: 10.13009/EUCASS2025-004
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Direct Numerical Simulation of a Supercritical Planar Jet
Leandro B. Magalh˜aes⋆†¶‡ and Marco Zecchetto⋆ ...
DOI: 10.13009/EUCASS2025-005
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
SECONDARY INJECTION LOCATION INFLUENCE ON
DUAL-BELL NOZZLE TRANSITION BEHAVIOUR
Brian LEGROS⋆ , Luc LEGER⋆† ...
DOI: 10.13009/EUCASS2025-007
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
A Method for Measuring the Leakage of Oxygen and Helium
using Standard Gas Flow Rates in Cryogenic Valves
Joongyoup ...
DOI: 10.13009/EUCASS2025-008
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
NUMERICAL SIMULATION OF BIRD-ENGINE BLADES
STRIKE USING SPH METHODE
KADA ZEMANI* and HANA SLAMANI†
* Ecole ...
DOI: 10.13009/EUCASS2025-009
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Estimation of the mechanism of consecutive hard starts in
bipropellant thrusters
Yoshiki Matsuura*† and ...
DOI: 10.13009/EUCASS2025-010
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Advanced Non-Adiabatic Flamelet-based Combustion and
Heat Transfer Model for Rocket Engine Thrust Chambers
Marvin ...
DOI: 10.13009/EUCASS2025-011
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Enabling Robust, Real-Time Verification of Vision-Based
Navigation through View Synthesis
Marius Neuhalfen1,2,3† ...
DOI: 10.13009/EUCASS2025-012
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Experimental Investigation of Propeller Aerodynamic
Derivatives
Jiří Čečrdle*†
* VZLU AEROSPACE, a.s.
Beranových ...
DOI: 10.13009/EUCASS2025-014
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Parametric Occupant Safety Assessment into the Aircraft
Preliminary Design Process Chain
Leonardo Marconi*† ...
DOI: 10.13009/EUCASS2025-015
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
UNSTEADY SIMULATION OF ICED SWEPT WINGS
USING ANISOTROPIC SUBGRID MODE BASED IDDES
METHOD
Ziyu Zhou1, ...
DOI: 10.13009/EUCASS2025-016
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Optimization of Hydrogen Semi-BWB type Airliner based on
International Air-route Market Performance
Jaesan ...
DOI: 10.13009/EUCASS2025-017
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Accelerating Space Mission Thermal Analysis: a Deep
Learning Framework for Rapid Temperature Prediction ...
DOI: 10.13009/EUCASS2025-020
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Deep Space Transfer Vehicle
Michael Paluszek, Josephine Kwok, Joyce Mo and Ian Jimenez
This paper presents ...
DOI: 10.13009/EUCASS2025-024
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Experimental Investigation of Solid Rocket Motors for a
Student Sounding Rocket
Yannick Lecomte1,2† , ...
DOI: 10.13009/EUCASS2025-026
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Space Rapid Transit: Reusable, Two Stage to Orbit, Launch
Vehicle with a Hypersonic First Stage
Joyce ...
DOI: 10.13009/EUCASS2025-027
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
ELECTRON BEAM PERFORATION AND JOINING OF
METALLIC SUCTION SHEETS WITH PRE-APPLIED
ADHESIVE TO CORE STRUCTURES ...
DOI: 10.13009/EUCASS2025-028
11ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Large-Eddy Simulation of a Rocket Nozzle Undergoing End
Effects
F. Burdairon'ç , G. Daviller', C. E. Tinneyæ ...