Use of experimental separation limits in the theoretical design of V/STOL inlets-Reference-Cited by-同舟云学术

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Use of experimental separation limits in the theoretical design of V/STOL inlets

Published:1977-07-11 Issue: Volume: Page:
ISSN:
Container-title:13th Propulsion Conference
language:
Short-container-title:

Author:

BOLES M.¹,STOCKMAN N.²

Affiliation:

1. Indiana Institute of Technology, Fort Wayne, Ind.

2. NASA, Lewis Research Center, Wind Tunnel and Flight Div., Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1977-878

Reference12 articles.

1. Albers, J. A. '*TheoreticzIand ExperimentInternal.Flow Characteristics of a 13.97-Centimeter-Diameter Inlet at STOL Takeoff and Approach Conditions,('NASA TND7185, 1973.

2. ' ' ' mental and Theoretical 13ounda.ry-Layer Separationfor Inlets at Incidence An.gleat Low-SpeedConditions,'' NASA TM X-3194, 1975.

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. Investigation of tangential blowing applied to a subsonic V/STOL inlet;Journal of Aircraft;1983-11

2. Experimental and analytical results of tangential blowing applied toa subsonic V/STOL inlet;18th Joint Propulsion Conference;1982-06-21

3. Prediction Methods for Jet V/STOL Propulsion Aerodynamics;Journal of Aircraft;1978-02

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