Control of Forebody Vortex Orientation to Enhance Departure Recovery of Fighter Aircraft
- 1 October 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (10) , 812-819
- https://doi.org/10.2514/3.61562
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Control of forebody vortex orientation to alleviate side forcesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Influence of spin rate on side force of an axisymmetric bodyAIAA Journal, 1978
- Nonlinearities in missile aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Prediction of aerodynamic out-of-plane forces on ogive-nosed circular cylindersJournal of Spacecraft and Rockets, 1977
- Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic streamJournal of Fluid Mechanics, 1976
- Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolutionAIAA Journal, 1970