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

Author:

Cedar R. D.,Stow P.

Publisher

Wiley

Subject

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

Reference10 articles.

1. ‘A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial- and mixed-flow types’, NACA TN2604, 1952.

2. and , Supercritical Wing Sections III, Lecture notes in economics and mathematical systems, Vol. 150, Springer-Verlag, New York 1975.

3. ‘Design of two-dimensional channels with prescribed velocity distributions along the channel walls’, NACA Rep No 1115, 1953.

4. ‘Computation of supercritical compressor and turbine cascades with a design method for transonic flows’, ASME 79-GT-30.

5. ‘The calculation of steady and unsteady transonic flow in cascades’, Cambridge University Engineering Department CUED/A-Turbo/TR118, 1982.

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