Universal scaling laws for nose bluntness effects on hypersonic unsteady aerodynamics
- 1 December 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (12) , 2222-2227
- https://doi.org/10.2514/3.5519
Abstract
No abstract availableThis publication has 7 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
- NOSE BLUNTNESS, CONE ANGLE, AND MACH NUMBER EFFECTS ON THE STABILITY DERIVATIVES OF SLENDER CONESPublished by Defense Technical Information Center (DTIC) ,1967
- Effect of nose bluntness on the hypersonic unsteady aerodynamics of an ablating re-entry body.Journal of Spacecraft and Rockets, 1967
- An application of automatic carpet plotting to wind-tunnel data reduction.Journal of Spacecraft and Rockets, 1967
- Similitute of Hypersonic Real-Gas Flows Over Slender Bodies with Blunted NosesJournal of the Aerospace Sciences, 1959