An Experimental Investigation of the Flowfield around a Yawed Cone
Open Access
- 1 June 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (6) , 1074-1081
- https://doi.org/10.2514/3.49918
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Laminar boundary layer on a cone at incidence in supersonic flowAIAA Journal, 1971
- Investigation of the leeward side of a delta wing at hypersonic speeds.Journal of Spacecraft and Rockets, 1969
- Hypersonic viscous interaction on slender cones.AIAA Journal, 1968
- Inviscid flowfield about a pointed cone at an angle of attack.AIAA Journal, 1967
- H. Supersonic Flows with Shock WavesPublished by Walter de Gruyter GmbH ,1954