Oil flow separation patterns on an ogive forebody
- 1 April 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (4) , 550-556
- https://doi.org/10.2514/3.8112
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976