Follow
Jeroen P. J. P. Van den Eynde
Jeroen P. J. P. Van den Eynde
Verified email at esa.int
Title
Cited by
Cited by
Year
Numerical simulations of transition due to isolated roughness elements at Mach 6
JPJP Van den Eynde, ND Sandham
AIAA Journal 54 (1), 53-65, 2016
272016
SNAPPSHOT: SUITE FOR THE NUMERICAL ANALYSIS OF PLANETARY PROTECTION
F Letizia, C Colombo, J Van den Eynde, R Armellin, R Jehn
6th International Conference on Astrodynamics Tools and Techniques, 2016
162016
Intermittency-Based Transition Model with Local Empirical Correlations
J Van den Eynde, J Steelant, A Passaro
21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017
82017
Numerical Simulation of Roughness-Induced Instability Growth and Transition at Mach 6
JPJP Van den Eynde, ND Sandham
7th AIAA Theoretical Fluid Mechanics Conference, 2014
82014
Compressibility and temperature effects on turbulent spot growth
J Van den Eynde, J Steelant
Proceedings of HiSST, 2018
72018
Ceramic strut injection technologies for high-speed flight
M Kuhn, M Bouchez, B Le Naour, JF Justin, J Van den Eynde, J Steelant
21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017
72017
SNAPPshot ESA planetary protection compliance verification software Final report V1
C Colombo, F Letizia, J Van Der Eynde
Univ. of Southampton, Tech. Rept. ESA-IPL-POM-MB-LE-2015-315, 2016
72016
B-plane visualisation tool for uncertainty evaluation
F Letizia, C Colombo, J Van den Eynde, R Jehn
26th AAS/AIAA Space Flight Mechanics Meeting, 2016
62016
Characterization of SRM plumes with alumina particulate in subscale testing: Fundamental outline and first results of the ESA-EMAP project
D Saile, D Allofs, V Kühl, L Steffens, A Gülhan, M Beversdorff, W Förster, ...
CEAS Space Journal 13, 247-268, 2021
52021
Stability and transition of the flow behind isolated roughness elements in hypersonic boundary layers
J Van den Eynde
University of Southampton, 2015
52015
Space Rider Observer Cube – SROC: a CubeSat mission for proximity operations demonstration
Corpino, S., G Ammirante, G Daddi, F Stesina, F Corradino, A Basler, ...
73rd International Astronautical Congress (IAC), Paris, France, 2022
42022
Test facility to investigate plume-regolith interactions
C White, H Zare-Behtash, K Kontis, T Ukai, J Merrifield, D Evans, I Coxhill, ...
Unitversity of Glasgow, 2019
32019
Overview to the esa-emap project: Characterization of srm plumes with alumina particulate in subscale testing
D Saile, D Kerkhoff, V Kühl, L Steffens, A Gülhan, M Beversdorff, ...
32019
An analysis tool for boundary layer and correlation-based transition onset assessment on generic geometries
JP Hoffmann, J Van den Eynde, J Steelant
CEAS Space Journal 15 (6), 923-945, 2023
22023
CFD computations of orbital and super-orbital Re-entry heating on primitive shapes
J Van den Eynde, S Lemmens
1st International Conference on Flight Vehicles, Aerothermodynamics, and Re …, 2019
22019
Particle size in srm plume: Assessment of collection method
F Maggi, S Carlotti, L Galfetti, D Saile, A Gulhan, M Liljedahl, ...
8th European Conference for Aerospace Sciences (EUCASS 2019), 1-10, 2019
22019
Two-equation transition model based on intermittency and empirical correlations
J Van den Eynde, J Steelant
Proceedings of HiSST, 2018
22018
NUMERICAL INVESTIGATION OF ROUGHNESS-INDUCED TRANSITION AT MACH 6 IN THE EUROPEAN ATLLAS-2 PROGRAMME
JPJP Van den Eynde, ND Sandham
8th European Symposium on Aerothermodynamics for Space Vehicles, 2015
22015
Linearly combined transition model based on empirical spot growth correlations
M Karsch, J Van den Eynde, J Steelant
CEAS Space Journal 15 (6), 947-958, 2023
12023
Experiments for collection and characterization of particles exiting from solid propellant rocket nozzles
F Maggi, S Carlotti, D Saile, A Guelhan, M Liljedahl, N Wingborg, ...
AIAA Propulsion and Energy 2020 Forum, 3932, 2020
12020
The system can't perform the operation now. Try again later.
Articles 1–20