Advances in Supersonic Configuration Design Methods
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57882
Reference16 articles.
1. Aircraft aerodynamic design and evaluation methods
2. Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex Configurations
3. An improved higher order panel method for linearized supersonic flow
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2. Evaluation of NCOREL, PAN AIR, and W12SC3 for supersonic wing pressures;Journal of Aircraft;1984-10
3. Application of panel methods to external stores at supersonic speeds;Journal of Aircraft;1983-02
4. A Subsonic Panel Method for Iterative Design of Complex Aircraft Configurations;Journal of Aircraft;1982-10
5. An optimal-surface-transpiration subsonic panel-method for iterative design of complex aircraft configurations;14th Fluid and Plasma Dynamics Conference;1981-06-23
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