Symmetric Body Vortex Wake Characteristics in Supersonic Flow
- 1 November 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (11) , 1289-1297
- https://doi.org/10.2514/3.50884
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- An investigation of separated flow about a hemisphere-cylinder at incidence in the Mach number range from 0.6 to 1.5Published by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Prediction of Roll Moments on Finned Bodies in Supersonic FlowJournal of Spacecraft and Rockets, 1975
- Aerodynamics of Finned Missiles at High Angle of AttackAIAA Journal, 1971
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971
- Investigation of Normal Force Distributions and Wake Vortex Characteristics of Bodies of Revolution at Supersonic SpeedsJournal of the Aerospace Sciences, 1959