Complementing numerical simulation methods with classical analytical techniques
Author:
Affiliation:
1. Boeing Co., Saint Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2486
Reference21 articles.
1. Solution of the Euler equations for airfoils using asymptotic methods
2. Verhoff, A., Stookesberry,D., andCain,A.B. "An Efficient Approach to Optimal Aerodynamic Design Part I: Analytic Geometry and Aerodynamic Sensitivities," AIAAPaperNo.93-0099,Jan.1993.
3. A new approach for efficient construction of asymptotic solutions of the two-dimensional Euler equations
4. Verhoff, A., Chen, H. H., Cebeci, T., and Michal, T. "An Accurate and Efficient Interactive Boundary Layer Method for Analysis andDesign ofAirfoils," AIAA Paper No.96-0328,Jan.1996.
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1. Verification and validation in computational fluid dynamics;Progress in Aerospace Sciences;2002-04
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