A Sensitivity Equation Method for Compressible Subsonic Laminar Airfoil Flows
Author:
Affiliation:
1. Ecole Polytechnique de Montreal
2. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4601
Reference16 articles.
1. 2Limache, A. C., Aerodynamic Modeling Using Computational Fluid Dynamics and Sensitivity Equations, Ph.D. thesis,Virginia Polytechnic Institute and State University, Blacksburg, VA, 2000.
2. A general continuous sensitivity equation formulation for complex flows
3. A continuous sensitivity equation method for flows with temperature dependent properties
4. Sensitivity and uncertainty analysis for variable property flows
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1. Application of a sensitivity equation method to compressible subsonic impinging jets;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
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