Analysis of Increased Compression Through Area Constriction on Ejector-Rocket Performance
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.26915
Reference33 articles.
1. Supersonic Air Ejectors
2. Optimal Supersonic Ejector Designs
3. Limitation of Ejector Performance Due to Exit Choking
4. Optimum Performance for a Single-Stage Gaseous Ejector
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