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Numerical Airfoil Optimization Using a Reduced Number of Design Coordinates PDF

22 Pages·2008·0.81 MB·English
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by Unknow| 2008| 22 pages| 0.81| English

About Numerical Airfoil Optimization Using a Reduced Number of Design Coordinates

minimize or maximize a prescribed design objective subject to constraints .. Case I - Lift Maximization, M = 0.1, a = 6' - Figure 3 shows results.

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Author:Unknown
Publication Year:2008
Pages:22
Language:English
File Size:0.81
Format:PDF
Price:FREE
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