Aerodynamic performance of scarf inlets-Reference-Cited by-同舟云学术

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Aerodynamic performance of scarf inlets

Published:1979-01-15 Issue: Volume: Page:
ISSN:
Container-title:17th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

ABBOTT J.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-380

Reference7 articles.

1. tic Performance of a Scoop Inlet," NASA TP-1028, 1977. 3, Yuska, J., Diedrich, J. H., and Clough, N. "Lewis 9- by 15-Foot V/STOL

2. Wind Tunnel.'' NASA TM X-2305, 1971. 4. Luidens, R. W., and Abbott, J. M. "Incidence Angle Bounds for Lip Flow

3. 77-1354, Oct. 1977.

4. Separation of Three 13-97-Centimeter-Diameter Inlets,I' NASA TM

5. v X-3351, 1976.

Cited by 4 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. Impact of Droop and Scarf on the Aerodynamic Performance of Compact Aero-Engine Nacelles;AIAA Scitech 2020 Forum;2020-01-05

2. Validation of WIND for a series of inlet flows;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

3. High speed test results of subsonic, turbofan scarf inlets;29th Joint Propulsion Conference and Exhibit;1993-06-28

4. A NUMERICAL ANALYSIS APPLIED TO HIGH ANGLE OF ATTACK THREE-DIMENSIONAL INLETS;22nd Joint Propulsion Conference;1986-06-16

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