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 | 38 | 2018 |
Basics of plume impingement analysis for small chemical and cold gas thrusters G Dettleff, M Grabe Models and computational methods for rarefied flows, 2011 | 22 | 2011 |
A kinetic Fokker–Planck approach to model hard-sphere gas mixtures C Hepp, M Grabe, K Hannemann Physics of Fluids 32 (2), 2020 | 17 | 2020 |
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 | 12 | 2018 |
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 | 11 | 2010 |
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 | 10 | 2020 |
Status and future of research on plume induced contamination M Grabe, CE Soares Proceedings of the International Astronautical Congress, IAC, 2019 | 10 | 2019 |
Comparison of computed free thruster plume expansion to experiments M Grabe, G Dettlef, K Hannemann Space propulsion conference, 2014 | 10 | 2014 |
Experimental Characterization of a Scalable Pulsed Magnetoplasmadynamic Propulsion System M Lau, M Grabe, G Herdrich | 8 | 2014 |
A kinetic Fokker–Planck approach for modeling variable hard-sphere gas mixtures C Hepp, M Grabe, K Hannemann AIP Advances 10 (8), 2020 | 7 | 2020 |
Flow characteristics of monopropellant micro-scale planar nozzles DT Banuti, M Grabe, K Hannemann Aerospace Science and Technology 86, 341-350, 2019 | 7 | 2019 |
Steady shock refraction in hypersonic ramp flow D Banuti, K Hannemann, M Grabe 17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011 | 7 | 2011 |
Non-equilibrium parameter for a hybrid Fokker-Planck/DSMC scheme C Hepp, M Grabe, K Hannemann AIP Conference Proceedings 2132 (1), 2019 | 6 | 2019 |
Impact of nozzle separation on the plumes of two parallel thrusters M Grabe, G Dettleff, K Hannemann AIP conference proceedings 1786 (1), 2016 | 6 | 2016 |
STG-CT: High-vacuum plume test facility for chemical thrusters M Grabe Journal of large-scale research facilities JLSRF 2 (A86), 1-5, 2016 | 4 | 2016 |
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 | 4 | 2014 |
Response of the Patterson probe in the transition flow regime M Grabe AIP Conference Proceedings 1501 (1), 1188-1194, 2012 | 4 | 2012 |
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 | 3 | 2013 |
A Voronoi Grid and a Particle Tracking Algorithm for DSMC F Stollmeier, M Grabe AIP Conference Proceedings 1333, 331, 2011 | 3 | 2011 |
Numerical simulation of nitrogen nozzle expansion using kinetic and continuum approaches M Grabe 59th International Astronautical Conference 2008, 2008 | 3 | 2008 |