Effects of nose bluntness, angle of attack, and oscillation amplitude on hypersonic unsteady aerodynamics of slender cones
- 19 January 1970
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Dynamic stability problems associated with flare stabilizers and flap controlsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Effect of boundary-layer transition on vehicle dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Unsteady aerodynamics of an ablating flared body of revolution including effect of entropy gradient.AIAA Journal, 1968
- Effect of nose bluntness on hypersonic unsteady aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- A destabilizing effect of severe nose bluntness.Journal of Spacecraft and Rockets, 1967
- NOSE BLUNTNESS, CONE ANGLE, AND MACH NUMBER EFFECTS ON THE STABILITY DERIVATIVES OF SLENDER CONESPublished by Defense Technical Information Center (DTIC) ,1967