Treatment of supersonic configurations by an updated low-order panelmethod
Author:
Affiliation:
1. Messerschmitt-Bolkow-Blohm GmbH, Ottobrunn, Federal Republic of Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48252
Reference23 articles.
1. 2Weiland C Calculation of Three Dimensional Stationary Supersonic Flowfields by Applying the Progonka Process to a Conservative Formulation of the Governing Equations Journal of Computational Physics, Vol29Nov 1978pp173198
2. 4Eberle A Methods for Solving Euler s Equations for Airfoil and Intake Flow ' Notes on Numerical Fluid Mechanics Vol 5 1982, pp 77 86
3. 5Morino L Chen L T and Suciu E O Steady and Oscillatory Subsonic and Supersonic Aerodynamics Around Complex Configurations AIAA Journal Vol 13, March 1975 pp 368374
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1. Linear Aerodynamics of Wings and Bodies;High Angle of Attack Aerodynamics;1992
2. A Subsonic Panel Method for Design of 3-Dimensional Complex Configurations with Specified Pressure Distribution;Panel Methods in Fluid Mechanics with Emphasis on Aerodynamics;1988
3. HISSS — A Higher-order Panel Method for Subsonic and Supersonic Attached Flow about Arbitrary Configurations;Panel Methods in Fluid Mechanics with Emphasis on Aerodynamics;1988
4. Application of HISSS panel code to a fighter-type aircraft configuration at subsonic and supersonic speeds;5th Applied Aerodynamics Conference;1987-08-17
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