Response surface approach to aerodynamic optimization design of helicopter rotor blade-Reference-Cited by-同舟云学术

Response surface approach to aerodynamic optimization design of helicopter rotor blade

Published:2005 Issue:1 Volume:64 Page:125-142
ISSN:0029-5981
Container-title:International Journal for Numerical Methods in Engineering
language:en
Short-container-title:Int. J. Numer. Meth. Engng

Author:

Sun Hyosung,Lee Soogab

Publisher

Wiley

Subject

Applied Mathematics,General Engineering,Numerical Analysis

Reference19 articles.

1. Influence of Tip Shape, Chord, Blade Number, and Airfoil on Advanced Rotor Performance

2. , , , . Multilevel decomposition approach to integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades. Presented at AHS Aeromechanics Specialists Conference, San Francisco, CA, 1994.

3. Application of numerical optimization methods to helicopter design problems: a survey. NASA TM 86010, 1984.

4. Preliminary structural design of composite main rotor blades for minimum weight. NASA TP 2730, 1987.

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