The role of a mixed design and analysis method in a turbomachinery blade design system-Reference-Cited by-同舟云学术

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The role of a mixed design and analysis method in a turbomachinery blade design system

Published:1986-01 Issue:1 Volume:2 Page:91-99
ISSN:0748-8025
Container-title:Communications in Applied Numerical Methods
language:en
Short-container-title:Commun. Appl. Numer. Methods

Author:

Ceder R. D.,Stow P.

Publisher

Wiley

Subject

General Engineering

Reference6 articles.

1. and . ‘Supercritical wing section III’, In Lecture Notes in Economics and Mathematical System, vol. 150, Springer Verlag, New York, 1975.

2. ‘The calculation of steady and unsteady transonic flow in cascades’, Cambridge Univ. Eng. Dept., CUED/A - Turbo/TR118 (1982).

3. A finite element method for the solution of two-dimensional transonic flows in cascades

4. The addition of quasi-three-dimensional terms into a finite element method for transonic turbomachinery blade-to-blade flows

5. Private communication.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Computational methods for aerodynamic shape design;Mathematical and Computer Modelling;1994-12

2. Aerodynamic shape design and optimization - Status and trends;Journal of Aircraft;1992-11

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