Numerical Investigation of the Application of Porous Material in Tandem Nozzle Supersonic Wind Tunnels (AIAA 2017-2125)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
2017-01-01
12 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Investigation Of Diffusers For Two Stream Supersonic Wind Tunnels (AIAA 2016-0047)
British Library Conference Proceedings | 2016
|A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels (AIAA 2016-3802)
British Library Conference Proceedings | 2016
|