Computation of nonlinear supersonic potential flow over three-dimensional surfaces
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, New York
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44894
Reference18 articles.
1. THEORETICAL AND EXPERIMENTAL STUDIES OF CAMBERED AND TWISTED WINGS OPTIMIZED FOR FLIGHT AT SUPERSONIC SPEEDS
2. A study of the inviscid flow about conically cambered delta wings
3. Numerical Procedure for the Computation of Irrotational Conical Flows
4. The nonlinear supersonic potential flow over delta wings
5. Opportunities for supersonic performance gains through non-linear aerodynamics
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1. Full-potential analysis of a supersonic delta wing/body;Journal of Aircraft;1989-03
2. Experimental flowfield visualization of a high alpha wing at Mach 1.62;Journal of Aircraft;1987-05
3. Application of NCOREL to aircraft configurations;4th Applied Aerodynamics Conference;1986-06-09
4. Application of a full potential method for predicting supersonic flowfields and aerodynamic characteristics;Journal of Spacecraft and Rockets;1986-01
5. The computational treatment of supersonic wake flows in INCOREL;23rd Aerospace Sciences Meeting;1985-01-14
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