Exhaust plumes from nozzles with wall boundary layers.
- 1 October 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (10) , 1143-1147
- https://doi.org/10.2514/3.29439
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Highly underexpanded jet structure - Exact and approximate calculations.AIAA Journal, 1967
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- The Turbulent Boundary LayerPublished by Elsevier ,1956
- The Analytical Design of an Axially Symmetric Laval Nozzle for a Parallel and Uniform JetJournal of the Aeronautical Sciences, 1949