Effect on Slender Vehicle Dynamics of Change from Spherical to Conical Nose Bluntness
- 1 June 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (6) , 435-440
- https://doi.org/10.2514/3.61707
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Conical nose shape effects on drag and static stability at Mach 10.Journal of Spacecraft and Rockets, 1972
- Comparison of free-flight experimental results with theory on the nonlinear aerodynamic effects of bluntness for slender cones at Mach number 17AIAA Journal, 1971
- Effects of nose bluntness, angle of attack, and oscillation amplitude on hypersonic unsteady aerodynamics of slender conesAIAA Journal, 1971
- Theoretical and experimental study of supersonic steady flow around inclined bodies of revolutionAIAA Journal, 1970
- Universal scaling laws for nose bluntness effects on hypersonic unsteady aerodynamicsAIAA Journal, 1969
- Pressure correlation for blunted slender cones.AIAA Journal, 1969
- Unsteady aerodynamics of an ablating flared body of revolution including effect of entropy gradient.AIAA Journal, 1968