Wind tunnel investigations for the flat spin of slender bodies at high angles of attack
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Steady and Unsteady Vortex-Induced Asymmetric Loads on Slender VehiclesJournal of Spacecraft and Rockets, 1981
- Side-Force Alleviation on Slender, Pointed Forebodies at High Angles of AttackJournal of Aircraft, 1979
- A Subsonic High-Angle-of-Attack Flow Investigation at Several Reynolds NumbersAIAA Journal, 1978
- Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic streamJournal of Fluid Mechanics, 1976
- On vortex shedding from a circular cylinder in the critical Reynolds number régimeJournal of Fluid Mechanics, 1969