A NUMERICAL ANALYSIS APPLIED TO HIGH ANGLE OF ATTACK THREE-DIMENSIONAL INLETS-Reference-Cited by-同舟云学术

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A NUMERICAL ANALYSIS APPLIED TO HIGH ANGLE OF ATTACK THREE-DIMENSIONAL INLETS

Published:1986-06-16 Issue: Volume: Page:
ISSN:
Container-title:22nd Joint Propulsion Conference
language:
Short-container-title:

Author:

HWANG D.P.¹

Affiliation:

1. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CLEVELAND, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1627

Reference18 articles.

1. Miller, B.A., Dastoli, B.J., and Wesoky, H.L. "Effect of Entry-Lip Design on Aerodynamics and Acoustics of High-Throat Mach Number Inlets for the Quiet, Clean, Short-Haul Experimental Engine,''NASA TM-X-3222, 1975.

2. !red Fan at High Angles of 70, 1977.

3. Aerodynamic performance of scarf inlets

Cited by 1 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. Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at Mach 0.2;27th Joint Propulsion Conference;1991-06-24

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