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   ESDU 01025▹

   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.

   standard by Engineering Sciences Data Unit, 04/01/2001.

   Languages: English

   Priced From:

   • $260 Secure PDF
   • $325 Printed Edition

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