Examples of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Design Point

Examples of the Application of Constrained Multivariate Optimisation Techniques to the Design of Aerofoil Sections. Design Point : Single,Geometry Var: LE and TE Flaps,Initial Aerofoil: Combat Aircraft Section,CFD: BVGK (inviscid),Euler Code. 00023

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Product details

  • Loose-leaf
  • IHS ESDU
  • ESDU International PLC
  • United Kingdom
  • 1862461260
  • 9781862461260