Dynamic simulation of supersonic inlet and engine-Reference-Cited by-同舟云学术

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Dynamic simulation of supersonic inlet and engine

Published:1964-08-10 Issue: Volume: Page:
ISSN:
Container-title:Transport Aircraft Design and Operations Meeting
language:
Short-container-title:

Author:

CHUN K.¹,SWANSON D.¹

Affiliation:

1. BOEING CO., AIRPLANE DIV., RENTON, WASH.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1964-598

Reference13 articles.

1. Bowditch, D. N., and Wilcox, F.A. 'Vyzamic Response ofa Supersonic Diffuser to Bypass and Spike Oscillation, "NASA TMX-10, August 1959 (Cod.)

2. Kopal, Z. "Tables of Sqersonic Flow Around Cones,I' Tech Report No. 1, Dept. of Electrical Engineering, Center of Analysis, MIT, 1947

3. Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic Transports

Cited by 3 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. Turbofan Volume Dynamics Model for Investigations of Aero-Propulso-Servo-Elastic Effects in a Supersonic Commercial Transport;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

2. Inlet dynamics and compressor surge;Journal of Aircraft;1971-04

3. A control system concept for an axisymmetric supersonic inlet;4th Propulsion Joint Specialist Conference;1968-06-10

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