Critical states and flow structure on a 65-deg delta wing
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46944
Reference16 articles.
1. Modeling aerodynamic discontinuities and onset of chaos in flight dynamical systems
2. 5Kaplan, W., Ordinary Differential Equations, 1st ed.Addison-Wesley, Reading, MA, 1958, pp.414-470.
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