Comparison of free-flight experimental results with theory on the nonlinear aerodynamic effects of bluntness for slender cones at Mach number 17
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (3) , 473-478
- https://doi.org/10.2514/3.6205
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Comparison of free-flight experimental results with theory on the nonlinear aerodynamic effects of bluntness for slender cones at Mach number 17Published by American Institute of Aeronautics and Astronautics (AIAA) ,1970
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- Effect of nose bluntness on hypersonic unsteady aerodynamics.Journal of Spacecraft and Rockets, 1969
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- THE UNSTEADY FLOW FIELD ABOUT A RIGHT CIRCULAR CONE IN UNSTEADY FLIGHTPublished by Defense Technical Information Center (DTIC) ,1967
- Calculation of hypersonic flow over bodies of revolution at small angles of attackAIAA Journal, 1965
- ON THE FREE FLIGHT MOTION OF MISSILES HAVING SLIGHT CONFIGURATIONAL ASYMMETRIESPublished by Defense Technical Information Center (DTIC) ,1953