Prediction for the Separation Length of Two-Dimensional Sonic Injection with High-Speed Crossflow-Reference-Cited by-同舟云学术

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Prediction for the Separation Length of Two-Dimensional Sonic Injection with High-Speed Crossflow

Published:2017-03 Issue:3 Volume:55 Page:832-847
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wang Zhen¹,Jiang Chongwen¹,Gao Zhenxun¹,Lee Chunhian¹

Affiliation:

1. Beihang University, 100191 Beijing, People’s Republic of China

Funder

Aerospace Science & Technology Innovation Foundation of China Aerospace Science & Technology Corporation

Fundamental Research Funds for the Central Universities

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055194

Reference36 articles.

1. Investigation of Supersonic Jet Interaction With Hypersonic Cross Flow

2. Interaction of jet in hypersonic cross stream

3. Surface Pressure Measurements in Supersonic Transverse Injection Flowfields

4. Transverse jets and their control

5. The Interaction of Jets with Crossflow

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