Comparison of a Turbulent Boundary Layer Pressure Fluctuation Model to Hypersonic Cone Measurements (AIAA 2016-4047)
Applied aerodynamics (Conference)
01.01.2016
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
New LES of a Hypersonic Shock/Turbulent Boundary Layer Interaction (AIAA 2016-0346)
British Library Conference Proceedings | 2016
|Flight Test of the Phoenix-1A Hybrid Rocket (AIAA 2015-4047)
British Library Conference Proceedings | 2015
|DataCite | 1923