Diffuser performance of two-stream supersonic wind tunnels-Reference-Cited by-同舟云学术

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Diffuser performance of two-stream supersonic wind tunnels

Published:1989-08 Issue:8 Volume:27 Page:1124-1127
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Papamoschou Dimitri¹

Affiliation:

1. California Institute of Technology, Pasadena, California

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.10232

Reference6 articles.

1. Compound-Compressible Nozzle Flow

2. 3Cosner, R. R. "Experiments on Thin Airfoils Spanning a Transonic Shear Flow," Ph.D. Thesis,California Institute of Technology, Pasadena, CA, June 1976.

3. 4PapamOschou, D. "Experimental Investigation of Heterogeneous Compressible Shear Layers," Ph.D. Thesis,California Institute of Technology, Pasadena, CA, Dec. 1986.

4. Observations of supersonic free shear layers

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis on the optimal mixing pressure and efficiency limit of an ideal ejector;Energy Reports;2021-11

2. A study on the performance characteristics of two-stream supersonic diffusers;Aerospace Science and Technology;2019-12

3. Experimental Investigations of a Diffuser Start/Unstart Characteristics for Two Stream Supersonic Wind Tunnel;31st International Symposium on Shock Waves 2;2019

4. Investigation Of Diffusers For Two Stream Supersonic Wind Tunnels;54th AIAA Aerospace Sciences Meeting;2016-01-02

5. Zones in coflowing planar inviscid supersonic twin streams;AIAA Journal;1994-10

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