Application of a higher order panel method to realistic supersonic configurations
Author:
Affiliation:
1. Boeing Aerospace Co., Seattle, Wash.
2. Mississippi State University, University, Miss.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-274
Reference9 articles.
1. Boundary-Value Problem of Configurations with Compressible Free Vortex Flow
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Linear Aerodynamics of Wings and Bodies;High Angle of Attack Aerodynamics;1992
2. CFD Applications to Complex Configurations: A Survey;Applied Computational Aerodynamics;1990-01-01
3. Evaluation of methods for predicting complex aircraft flowfields;Journal of Aircraft;1988-05
4. 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
5. Prediction of the steady three-dimensional aerodynamics of a supersonic ramjet missile;21st Joint Propulsion Conference;1985-07-08
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