Computation of vortex breakdown on a rolling delta wing-Reference-Cited by-同舟云学术

Computation of vortex breakdown on a rolling delta wing

Published:1995-05 Issue:3 Volume:32 Page:686-688
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Gordiner Raymond E.¹

Affiliation:

1. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7913

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46777

Reference19 articles.

1. Aerodynamic design of supersonic cruise wings with a calibrated linearized theory

2. 3Amendola, A., Tognaccini, R., Boerstoel, J. W., and Kassies, A., Validation of a Multi-Block Euler Flow Solver with Propeller-Slipstream Flows, Vol.2, AGARD-CP-437,May 1988, pp.1-15.

3. Euler solutions for high-speed flow about complex three-dimensional configurations

4. Progress in the aerodynamic analysis of inviscid supersonic flow fields around complex aircraft configurations

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