The design of transonic aerofoils by a well-posed inverse method-Reference-Cited by-同舟云学术

The design of transonic aerofoils by a well-posed inverse method

Published:1986-02 Issue:2 Volume:22 Page:341-361
ISSN:0029-5981
Container-title:International Journal for Numerical Methods in Engineering
language:en
Short-container-title:Int. J. Numer. Meth. Engng.

Author:

Volpe G.,Melnik R. E.

Publisher

Wiley

Subject

Applied Mathematics,General Engineering,Numerical Analysis

Reference18 articles.

1. and , Supercritical Wing Sections, Springer Verlag, Berlin, 1972.

2. and , ‘Transonic shock-free airfoil design by an analytic hodograph method’, A.I.A.A. Paper 74-439 (1974).

3. , and , ‘Airfoil section drag reduction at transonic speeds by numerical optimization’, NASA TMX-73097 (Feb. 1976).

4. ‘Technique for developing design tools from the analysis methods of computational aerodynamics’, A.I.A.A. Paper 79-1529 (1979).

5. ‘An artificial viscosity method for the design of supercritical airfoils’, Research and Development Report C00-3077-158, Courant Inst. Math. Sci., New York Univ. (July 1979).

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