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Examples of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Design Point : Single,Upper and Lower Surfaces Geometry and Camber Line Variations,Initial Aerofoil: NACA 0012 and RAE 2822,CFD: BVGK. 01025

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Product Details
ESDU International PLC
1862461821 / 9781862461826
Loose-leaf
01/04/2001
United Kingdom