Conical nose shape effects on drag and static stability at Mach 10.
- 1 February 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (2) , 126-128
- https://doi.org/10.2514/3.30384
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Aerothermodynamic characteristics of slender ablating re-entry vehiclesJournal of Spacecraft and Rockets, 1971
- Comparison of free-flight experimental results with theory on the nonlinear aerodynamic effects of bluntness for slender cones at Mach number 17AIAA Journal, 1971