High-speed Flying Vehicle with Hypergeometrically Shaped Windward Aerodynamic Surface (AIAA 2015-3571)
AIAA international space planes and hypersonic systems and technologies conference
2015-01-01
14 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1914
Static Aeroelastic Model Assessment in the Transonic Regime (AIAA 2016-3571)
British Library Conference Proceedings | 2016
|British Library Conference Proceedings | 2007
|Aerodynamic Control Using Windward-Surface Plasma Actuators on a Separation Ramp
Online Contents | 2007
|