FLOW STEADINESS OVER A DOUBLE WEDGE AT MACH 7 INCLUDING EFFECT OF TRAILING EDGE EXPANSION (AIAA 2018-5388)
AIAA International Space Planes and Hypersonic Systems and Technolgies (Conference)
01.01.2018
24 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA-2006-5388 Satellite and Wireless Integration
British Library Conference Proceedings | 2006
|Airfoil Trailing-edge Noise Reduction using Flow Suction (AIAA 2018-2814)
British Library Conference Proceedings | 2018
|Trailing-Edge Noise in Slowly-Varying, Sheared Flow (AIAA 2018-2810)
British Library Conference Proceedings | 2018
|Active Flow Control for Trailing Edge Flap Separation (AIAA 2018-1799)
British Library Conference Proceedings | 2018
|