Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression-Reference-Cited by-同舟云学术

Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression

Published:2017-12 Issue:12 Volume:55 Page:4286-4295
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chen Hao¹,Tan Hui-Jun¹,Zhang Qi-Fan¹,Zhang Yue¹

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

China Postdoctoral Science Foundation

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056066

Reference21 articles.

1. Aircraft Propulsion Systems Technology and Design

2. OswatitschK. “Pressure Recovery in Missile in Reaction Propulsion at High Supersonic Speeds,” NACA TM-1140, 1947.

3. Aircraft Engine Design, Second Edition

4. FisherS. A.NealeM. C.BrooksA. J. “On the Sub-Critical Stability of Variable Ramp Intakes at Mach Numbers Around 2,” National Gas Turbine Establishment Rept. ARC-R/M-3711, Fleet, England, Feb. 1970.

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