Experimental flowfield visualization of a high alpha wing at Mach 1.62-Reference-Cited by-同舟云学术

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Experimental flowfield visualization of a high alpha wing at Mach 1.62

Published:1987-05 Issue:5 Volume:24 Page:335-341
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Pittman James L.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45450

Reference17 articles.

1. Vortex Flow Aerodynamics, Vol. I, NASA CP-2416, July 1986.

2. Vortex Flow Aerodynamics, Vol. II, NASA CP-2417, July 1986.

3. Vortex Flow Aerodynamics, Vol. Ill, NASA CP-2418, July 1986.

4. Opportunities for supersonic performance gains through non-linear aerodynamics

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. A planar Mie scattering visualization technique for turbo machinery application;Measurement Science and Technology;2007-10-19

2. Design and experimental verification of an equivalent forebody representation of flowing inlets;Journal of Aircraft;1989-12

3. An Euler analysis of leading-edge vortex flows on a forebody-strake at supersonic speeds;27th Aerospace Sciences Meeting;1989-01-09

4. Microtuft flow visualization at Mach 10 and 14 in the NSWC hypervelocity wind tunnel No. 9;27th Aerospace Sciences Meeting;1989-01-09

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