Supersonic flow in the second-throat ejector-diffuser system
Author:
Affiliation:
1. National Taiwan University, Taipei, Taiwan 10764, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26411
Reference18 articles.
1. Recent Development of a Jet-Diffuser Ejector
2. Thrust Augmenting Ejectors, Part I
3. Thrust augmenting ejectors, II
4. Design of Branched and Unbranched Axially Symmetrical Ducts with Specified Pressure Distribution
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