Aspects of the transpiration model for aerofoil design-Reference-Cited by-同舟云学术

Aspects of the transpiration model for aerofoil design

Published:1994-03-15 Issue:5 Volume:18 Page:509-528
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Int. J. Numer. Meth. Fluids

Author:

Yiu K. F. C.,Stow P.

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference6 articles.

1. A compatible mixed design and analysis finite element method for the design of turbomachinery blades

2. ‘An inverse transonic wing design method’, AIAA Paper 80-0330, 1980.

3. and , ‘A finite element inverse method for the design of turbomachinery blades’, ASME Paper 91-GT-80, 1991.

4. Fundamentals of Aerodynamics, McGraw-Hill, New York, 1984.

5. ‘Numerical methods of turbomachinery’, in and (eds), Recent Advances in Numerical Methods in Fluids, Vol. 1, Pineridge, Swansea, 1980, pp. 245-286.

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4. Airfoil design via transpiration and optimal control theory;Inverse Problems in Engineering;1996-08

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