Review of the Application of Hodograph Theory to Transonic Aerofoil Design and Theoretical and Experimental Analysis of Shock-free Aerofoils-Reference-Cited by-同舟云学术

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Review of the Application of Hodograph Theory to Transonic Aerofoil Design and Theoretical and Experimental Analysis of Shock-free Aerofoils

Published:1976 Issue: Volume: Page:109-133
ISSN:
Container-title:Symposium Transsonicum II
language:
Short-container-title:

Author:

Boerstoel J. W.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-81005-3_11.pdf

Reference29 articles.

1. Bers, L.: Mathematical aspects of subsonic and transonic gas dynamics, John Wiley and Sons Inc., New York (1958).

2. V. Mises, R., and H. Geiringer and G.S.S. Ludford: Mathematical theory of compressible fluid flow, Academic Press Inc., New York (1958).

3. Manwell, A.R.: The hodograph equations (An introduction to the mathematical theory of plane transonic flow), Oliver and Boyd, Edingburgh (1971).

4. Nieuwland, G.Y.: Transonic potential flow around a family of quasi-elliptical sections, NLR TR T 172 (1967).

5. Chaplygin, A.A.: On gas jets, NACA Techn. Mem. 1063 (1944).

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1. Optimum transonic airfoils based on the Euler equations;Computers & Fluids;1999-05

2. Oblique Flying Wing Studies;New Design Concepts for High Speed Air Transport;1997

3. Oblique flying wing aerodynamics;Theroretical Fluid Mechanics Conference;1996-06-17

4. Approximate solution of inverse shock-free transonic airfoil problem at zero incidence;Acta Mechanica;1987-12

5. New Method for Designing Shock-Free Transonic Configurations;AIAA Journal;1979-07

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