Supersonic near-wake afterbody boattailing effects on axisymmetric bodies
- 1 November 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 31 (6) , 1021-1028
- https://doi.org/10.2514/3.26553
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- The effect of expansion on the large scale structure of a compressible turbulent boundary layerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Two-stream, supersonic, wake flowfield behind a thick base. I - General featuresAIAA Journal, 1992
- The rapid expansion of a supersonic turbulent flow: role of bulk dilatationJournal of Fluid Mechanics, 1987
- Turbulence Measurements in a Compressible Reattaching Shear LayerAIAA Journal, 1984
- Effects of External Compression on an Axisymmetric Turbulent Near WakeAIAA Journal, 1978
- Subsonic Axisymmetric Near-Wake StudiesAIAA Journal, 1978
- Two-Dimensional Boat-Tailed Bases in Supersonic FlowAeronautical Quarterly, 1974
- A modified wall wake velocity profile for turbulent compressible boundary layers.Journal of Aircraft, 1973
- Optimization of Drag Minimums Including Effects of Flow SeparationJournal of Engineering for Industry, 1973
- Wave drag of optimum and other boat tailsJournal of Aircraft, 1970