Connection between leading-edge sweep, vortex lift, and vortex strength for delta wings-Reference-Cited by-同舟云学术

Connection between leading-edge sweep, vortex lift, and vortex strength for delta wings

Published:1990-05 Issue:5 Volume:27 Page:473-475
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hemsch Michael J.¹,Luckring James M.²

Affiliation:

1. PRC Aerospace Technologies Division, Hampton, Virginia

2. NASA Langley Research Center, Hampton, Virginia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.25305

Reference6 articles.

2. Three-dimensional hypersonic gas flow past slender bodies at high angles of attack

3. 5Wentz, W. H., and McMahon, M. C. "Further Experimental Investigations of Delta and Double-Delta Wing Flow Fields at Low Speeds, NASA CR-714, Feb. 1967.

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