A Potential Flow Design Method for Multicomponent Airfoil Sections-Reference-Cited by-同舟云学术

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A Potential Flow Design Method for Multicomponent Airfoil Sections

Published:1978-01 Issue:1 Volume:15 Page:47-52
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Kennedy J. L.¹,Marsden D.J.¹

Affiliation:

1. University of Alberta, Edmonton, Alberta, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.58311

Reference8 articles.

1. ^oldstein, A. W. and Jerison, M. "Isolated and Cascade Airfoils with Prescribed Velocity Distribution," NACA Technical Report No. 869, 1947.

2. 3Chen, A. W. "The Determination of the Geometries of Multiple Element Airfoils Optimised for Maximum Lift Coefficient," Ph.D. Thesis,University of Illinois, Urbana, Illinois, 1972.

3. Inverse Method for the Design of Multielement High-Lift Systems

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