Exhaust plumes from nozzles with wall boundary layers.
Author:
Affiliation:
1. Convair Division of General Dynamics, San Diego, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29439
Reference13 articles.
1. Highly underexpanded jet structure - Exact and approximate calculations.
2. Rapid expansion of a supersonic boundary layer and its application to the near wake.
3. Hypersonic boundary-layer separation and the base flow problem.
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