Base pressure measurements on slender cones with domed afterbodies.
- 1 August 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (8) , 1607-1609
- https://doi.org/10.2514/3.5442
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Stability of oscillating wedges and caret wings in hypersonic and supersonic flows.AIAA Journal, 1969
- Experimental studies on the lip shock.AIAA Journal, 1968
- Free-flight base pressure and heating measurements on sharp and blunt cones in a shock tunnel.AIAA Journal, 1967
- Effect of wave reflections on the unsteady hypersonic flow over a wedge.AIAA Journal, 1966
- Measurements of the turbulent near wake of a cone at Mach 6.AIAA Journal, 1966
- Hypersonic flow over an oscillating wedgeAIAA Journal, 1965
- Aerodynamic pitching derivatives of a wedge in hypersonic flowAIAA Journal, 1964
- INTRODUCTIONPublished by Elsevier ,1961
- On Weak Interaction of Strong Shock and Mach Waves Generated Downstream of the ShockJournal of the Aeronautical Sciences, 1952
- XVIII. The flow behind a stationary shockJournal of Computers in Education, 1949