Experimental-theoretical correlation of supersonic jet-on base pressure for cylindrical afterbodies
- 1 September 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 7 (5) , 474-477
- https://doi.org/10.2514/3.44201
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Analysis of the Axisymmetric Base-Pressure and Base-Temperature Problem with Supersonic Interacting Freestream-Nozzle Flows Based on the Flow Model of Korst, et al. Part III. A Computer Program and Representative Results for Cylindrical, Boattailed, or Flared AfterbodiesPublished by Defense Technical Information Center (DTIC) ,1970