An inverse calculation technique for quasi-three-dimensional turbomachinery cascades-Reference-Cited by-同舟云学术

An inverse calculation technique for quasi-three-dimensional turbomachinery cascades

Published:1993-09 Issue:2-3 Volume:57 Page:197-204
ISSN:0096-3003
Container-title:Applied Mathematics and Computation
language:en
Short-container-title:Applied Mathematics and Computation

Author:

Jenkins R.M.,Moore D.A.

Publisher

Elsevier BV

Subject

Applied Mathematics,Computational Mathematics

Reference9 articles.

1. An approximate design method for high-solidity blade elements in compressors and turbines;Stanitz;National Advisory Committee for Aeronautics Technical Note 2408,1951

2. A comprehensive method for preliminary design optimization of axial gas turbine stages;Jenkins,1982

3. Examination of axial-flow turbine blade-loading characteristics using diffusion parameters;Stewart,1967

4. The application of controlled-vortex aerodynamics to advanced axial flow turbines;Dorman;Transactions of the ASME Journal of Engineering for Power,1968

5. Reduction of end-wall effects in a small low-aspect-ratio turbine by radial work redistribution;Schlegel;Transactions of the ASME Journal of Engineering for Power,1976

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