A fast, e cient and reliable code for wing design has been developed at INTA coupling a residual-correction method by Bauer, McFadden and Garabedian to an inviscid solver for wing analysis in transonic ow. Smoothing procedures, including BΓ ezier cubic splines, are used to avoid irregularities of th
Inverse method with geometric constraints for transonic aerofoil design
β Scribed by J. M. J. Fray; J. W. Slooff; J. W. Boerstoel; A. Kassies
- Publisher
- John Wiley and Sons
- Year
- 1986
- Tongue
- English
- Weight
- 681 KB
- Volume
- 22
- Category
- Article
- ISSN
- 0029-5981
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