Compressibility effects on vortex breakdown onset above a 75-degree sweep delta wing
Author:
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
Reference22 articles.
1. Three-dimensional flow structure on delta wings at high angle-of-attack - Experimental concepts and issues
2. On the structure, interaction, and breakdown characteristics of slender wing vortices at subsonic, transonic, and supersonic speeds
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