Transonic flowfield in a supersonic nozzle with small throat radius of curvature.
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference14 articles.
1. TRANSONIC FLOW IN TWO-DIMENSIONAL AND AXIALLY-SYMMETRIC NOZZLES
2. Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic region
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