Influence of Contraction Section Shape and Inlet Flow Direction on Supersonic Nozzle Flow and Performance
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.61705
Reference16 articles.
1. Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic region
2. Transonic flowfield in a supersonic nozzle with small throat radius of curvature.
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