Design of supersonic airfoils by numerical optimization-Reference-Cited by-同舟云学术

Design of supersonic airfoils by numerical optimization

Published:1979-09 Issue:3 Volume:19 Page:417-427
ISSN:0045-7825
Container-title:Computer Methods in Applied Mechanics and Engineering
language:en
Short-container-title:Computer Methods in Applied Mechanics and Engineering

Author:

Dutt H.N.V.,Sreekanth A.K.

Publisher

Elsevier BV

Subject

Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference10 articles.

1. Wing sections with minimum drag at supersonic speeds;Drougge,1969

2. Airfoil profiles for minimum pressure drag at supersonic velocities-general analysis with application to linearized supersonic flow;Chapman;NACA rept. no. 1063,1952

3. Second order theory of optimum two-dimensional wings in supersonic flow including effects of friction;Miele,1963

4. An assessment of airfoil design by numerical optimization;Hicks;NASA TMX-3092,1974

5. Design of lowspeed airfoils by numerical optimization;Hicks;SAE paper 750524,1975

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3. Multifidelity, Multistrategy, and Multidisciplinary Design Optimization Environment;Journal of Aircraft;2012-09

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5. Wing Section Optimization for Supersonic Viscous Flow;Journal of Fluids Engineering;1998-03-01