Similarity in Vortex Asymmetries over Slender Bodies and Wings
- 1 September 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (9), 1370-1372
- https://doi.org/10.2514/3.60795
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Artificial Thickening of High Subsonic Mach Number Boundary LayersAIAA Journal, 1976
- 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
- Experimental evaluation of an injector system for powering a high Reynolds number transonic wind tunnelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950