A linear approach to the multi-parameter design of three-dimensional turbomachinery blades-Reference-Cited by-同舟云学术

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A linear approach to the multi-parameter design of three-dimensional turbomachinery blades

Published:1999-01-11 Issue: Volume: Page:
ISSN:
Container-title:37th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Shahpar S.¹,Lapworth B.¹,De Pablos T.¹,Taylor M.¹

Affiliation:

1. Rolls-Royce, plc, Derby, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-363

Reference15 articles.

1. r31 Doorly, D.J. and Peiro, J. "Supervised Parallel Genetic Algorithms in AerodynamicOptimisation", AIAA-97-1852, 1997.

2. Aly, S., Marconi, F., Ogot, M., Pelz, R. And Siclari, M. "Stochastic Optimization Applied to CFDShapeDesign",AIAA-95-1647-C? 1995.

3. i31 Narducci, R, Grossman,M., Valorani, M., Dadone, A and Haftb RT. "Optimization Methods for Non-Smoothor Noisy Objective Functions in Fluid DesignProblems",AIAA 95-1648CP,1995.

Cited by 1 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. Nonaxisymmetric Turbine End Wall Design: Part I— Three-Dimensional Linear Design System;Journal of Turbomachinery;1999-02-01

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