Unthrottled Flows with Complex Background Waves in Curved Isolators-Reference-Cited by-同舟云学术

Unthrottled Flows with Complex Background Waves in Curved Isolators

Published:2017-09 Issue:9 Volume:55 Page:2942-2955
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Huang He-xia¹,Tan Hui-jun¹,Sun Shu¹,Sheng Fa-jia¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Funder

priority academic program development of Jiangsu higher education institutions

Fundamental Research Funds for the Central Universities

Jiangsu Innovation Program for Graduate Education

National Nature Science Foundation of P.R.China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055735

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4. GnosA. V.WatsonE. C.SeebaughW. R., Sanator, R. J., and Decarlo, J. P. “Investigation of Flow Fields Within Large Scale Hypersonic Inlet Models,” NASA TN-D7150, 1973.

5. Experimental and numerical investigations on flow fields and performance of dual combustion ramjet

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