Measurements of a simulated rocket exhaust plume near the Prandtl-Meyer limiting angle
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27831
Reference12 articles.
1. Exhaust plumes from nozzles with wall boundary layers.
2. Effect of nozzle boundary layers on rocket exhaust plumes.
3. Analytical approximation for the flow from a nozzle into a vacuum.
4. Far field approximation for a nozzle exhausting into a vacuum.
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