Flight results showing the effect of mass addition on base pressure
- 1 September 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (9) , 1705-1707
- https://doi.org/10.2514/3.5971
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnelAIAA Journal, 1970
- Mean properties of the turbulent near wake of a slender body with and without base injection.AIAA Journal, 1969
- Base pressure results at M equals 4 using free-flight and sting-supported models.AIAA Journal, 1968
- Local flow effects on base pressure.AIAA Journal, 1968