Numerical Simulation of Ignition Process in Multi-cavity Combustors at High Supersonic Flight Condition (AIAA 2017-2186)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
01.01.2017
7 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Experimental Studies of Film Cooling in Supersonic Combustors (AIAA 2017-2267)
British Library Conference Proceedings | 2017
|Implicit Large-Eddy Simulation of a Supersonic Cavity (AIAA 2017-1477)
British Library Conference Proceedings | 2017
|DataCite | 1887
AIAA-2006-2186 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings
British Library Conference Proceedings | 2006
|