Rapid design space approximation for two-dimensional transonic aerofoil design
Author:
Affiliation:
1. British Aerospace (Operations) Ltd., Filton, Bristol BS12 7QW, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.47063
Reference13 articles.
1. Determination of aerodynamic sensitivity coefficients based on the three-dimensional full potential equation
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3. An Approximately Factored Incremental Strategy for Calculating Consistent Discrete Aerodynamic Sensitivity Derivatives
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1. Biobjective Design Optimization for Axial Compressors Using Tabu Search;AIAA Journal;2008-03
2. Airfoil Design Using a Genetic Algorithm and an Inverse Method;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
3. Aerodynamic Optimization Using Analytic Descriptions of the Design Space;Journal of Aircraft;1998-11
4. Optimization of low boom configuration of SST by genetic algorithm;29th AIAA, Fluid Dynamics Conference;1998-06-15
5. Inverse and Direct Airfoil Design Using a Multiobjective Genetic Algorithm;AIAA Journal;1997-09
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