Free-flight investigation of the aerodynamic characteristics of a cone at high Mach numbers
- 1 February 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (2) , 294-300
- https://doi.org/10.2514/3.5659
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- NOSE BLUNTNESS, CONE ANGLE, AND MACH NUMBER EFFECTS ON THE STABILITY DERIVATIVES OF SLENDER CONESPublished by Defense Technical Information Center (DTIC) ,1967
- THE UNSTEADY FLOW FIELD ABOUT A RIGHT CIRCULAR CONE IN UNSTEADY FLIGHTPublished by Defense Technical Information Center (DTIC) ,1967
- High amplitude dynamic stability characteristics of blunt 10-degree conesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966