Modification of subsonic wakes using boundary layer and base mass transfer
- 1 May 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (5) , 665-670
- https://doi.org/10.2514/3.8131
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Viscid-Inviscid Interaction of Incompressible Separated FlowsJournal of Applied Mechanics, 1976
- Theoretical prediction of base pressure for steady base flowProgress in Aerospace Sciences, 1973
- A New Wind-Tunnel Technique for Providing Simulation of Flight Base FlowJournal of Spacecraft and Rockets, 1971
- Correlation of Base Pressure and Wake Structure of Sharp- and Blunt-Nose Cones with Reynolds Number Based on Boundary-Layer Momentum ThicknessJournal of the Aerospace Sciences, 1959
- Interrelationship Between Boundary Layer and Base PressureJournal of the Aeronautical Sciences, 1951