Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attack
- 26 January 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Side forces on unyawed slender inclined aerodynamic bodiesJournal of Aircraft, 1975
- Prediction of Yawing Force at High Angle of AttackAIAA Journal, 1974
- Three-Dimensional Flow Separations on Aircraft and MissilesAIAA Journal, 1972
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971