Multidisciplinary optimization for gas turbine airfoil design-Reference-Cited by-同舟云学术

Multidisciplinary optimization for gas turbine airfoil design

Published:2000-06 Issue:3 Volume:8 Page:283-308
ISSN:1068-2767
Container-title:Inverse Problems in Engineering
language:en
Short-container-title:Inverse Problems in Engineering

Author:

Talya S. S.,Rajadas J. N.,Chattopadhyay A.

Publisher

Informa UK Limited

Subject

Applied Mathematics,Engineering (miscellaneous)

Link

http://www.tandfonline.com/doi/pdf/10.1080/174159700088027731

Reference26 articles.

1. Vogel, D. T. 1996. Navier-Stokes Simulation of the Flow Around a Leading Edge Film-Cooled Turbine Blade Including the Interior Cooling System and Comparison with Experimental Data. Proceedings of the International Gas. Turbine and Aeroengine Congress and Exhibition. June 10–131996, Birmingham, UK. Paper No. 96-GT-71

2. Eckert, E. R. G. 1983. Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades. Proceedings of the Tokyo International Gas Turbine Congress. October 24–281983, Tokyo, Japan. ASME. Paper No95-GT-2

3. Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces

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