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Martin Grabe
Martin Grabe
Bestätigte E-Mail-Adresse bei dlr.de
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Zitiert von
Zitiert von
Jahr
Assessment of the cubic Fokker–Planck–DSMC hybrid method for hypersonic rarefied flows past a cylinder
E Jun, MH Gorji, M Grabe, K Hannemann
Computers & Fluids 168, 1-13, 2018
382018
Basics of plume impingement analysis for small chemical and cold gas thrusters
G Dettleff, M Grabe
Models and computational methods for rarefied flows, 2011
222011
A kinetic Fokker–Planck approach to model hard-sphere gas mixtures
C Hepp, M Grabe, K Hannemann
Physics of Fluids 32 (2), 2020
172020
Cubic Fokker–Planck method for rarefied monatomic gas flow through a slit and an orifice
E Jun, M Grabe, K Hannemann
Computers & Fluids 175, 199-213, 2018
122018
Numerical simulation of nozzle flow into high vacuum using kinetic and continuum approaches
M Grabe, RD Boettcher, S Fasoulas, K Hannemann
New Results in Numerical and Experimental Fluid Mechanics VII: Contributions …, 2010
112010
Master equation approach for modeling diatomic gas flows with a kinetic Fokker-Planck algorithm
C Hepp, M Grabe, K Hannemann
Journal of Computational Physics 418, 109638, 2020
102020
Status and future of research on plume induced contamination
M Grabe, CE Soares
Proceedings of the International Astronautical Congress, IAC, 2019
102019
Comparison of computed free thruster plume expansion to experiments
M Grabe, G Dettlef, K Hannemann
Space propulsion conference, 2014
102014
Experimental Characterization of a Scalable Pulsed Magnetoplasmadynamic Propulsion System
M Lau, M Grabe, G Herdrich
82014
A kinetic Fokker–Planck approach for modeling variable hard-sphere gas mixtures
C Hepp, M Grabe, K Hannemann
AIP Advances 10 (8), 2020
72020
Flow characteristics of monopropellant micro-scale planar nozzles
DT Banuti, M Grabe, K Hannemann
Aerospace Science and Technology 86, 341-350, 2019
72019
Steady shock refraction in hypersonic ramp flow
D Banuti, K Hannemann, M Grabe
17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011
72011
Non-equilibrium parameter for a hybrid Fokker-Planck/DSMC scheme
C Hepp, M Grabe, K Hannemann
AIP Conference Proceedings 2132 (1), 2019
62019
Impact of nozzle separation on the plumes of two parallel thrusters
M Grabe, G Dettleff, K Hannemann
AIP conference proceedings 1786 (1), 2016
62016
STG-CT: High-vacuum plume test facility for chemical thrusters
M Grabe
Journal of large-scale research facilities JLSRF 2 (A86), 1-5, 2016
42016
Numerical investigation of two interacting parallel thruster-plumes and comparison to experiment
M Grabe, A Holz, S Ziegenhagen, K Hannemann
AIP Conference Proceedings 1628 (1), 581-588, 2014
42014
Response of the Patterson probe in the transition flow regime
M Grabe
AIP Conference Proceedings 1501 (1), 1188-1194, 2012
42012
Characterization of a Free-Molecular Pressure Probe employing Gas-Kinetic Simulation
M Grabe, G Dettleff, RD Boettcher, K Hannemann
New Results in Numerical and Experimental Fluid Mechanics VIII …, 2013
32013
A Voronoi Grid and a Particle Tracking Algorithm for DSMC
F Stollmeier, M Grabe
AIP Conference Proceedings 1333, 331, 2011
32011
Numerical simulation of nitrogen nozzle expansion using kinetic and continuum approaches
M Grabe
59th International Astronautical Conference 2008, 2008
32008
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