Base drag calculations in supersonic turbulent axisymmetric flows.
- 1 April 1973
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 10 (4) , 285-287
- https://doi.org/10.2514/3.27756
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Exploratory Analysis of Nonuniform Plug Nozzle FlowfieldsJournal of Spacecraft and Rockets, 1972
- Turbulent axisymmetric near-wake at Mach four with base injectionAIAA Journal, 1970
- Influence of initial flow direction on the turbulent base pressure in supersonic axisymmetric flowJournal of Spacecraft and Rockets, 1970
- Base pressure results at M equals 4 using free-flight and sting-supported models.AIAA Journal, 1968
- Determination of the turbulent base pressure in supersonic axisymmetric flow.Journal of Spacecraft and Rockets, 1968
- Cylindrical afterbodies in supersonic flow with gas ejection.AIAA Journal, 1967
- A time-dependent computational method for blunt body flows.AIAA Journal, 1966
- Base pressure measurements on sharp and blunt 9 deg cones at Mach numbers from 3.50 to 9.20.AIAA Journal, 1966