The influence of airfoil thickness and Reynolds number on separation-Reference-Cited by-同舟云学术

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The influence of airfoil thickness and Reynolds number on separation

Published:1994 Issue:2 Volume:33 Page:151-180
ISSN:0044-2275
Container-title:ZAMP Zeitschrift f�r angewandte Mathematik und Physik
language:en
Short-container-title:Z. angew. Math. Phys.

Author:

Cheng H. K.,Smith F. T.

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,General Physics and Astronomy,General Mathematics

Link

http://link.springer.com/content/pdf/10.1007/BF00944968.pdf

Reference38 articles.

1. I. H. Abbott and A. E. von Doenhoff,Theory of wing sections. Dover Publ, New York 1959.

2. S. Brodetsky, Proc. Roy. Soc. A102, 542 (1923).

3. O. R. Burggraf, AGARD paper no. 168, on flow separation. 1975.

4. O. R. Burggraf, Ohio State Univ. Res. Found., techn. rept 1 (1976).

5. T. Carleman, Arkiv för Matematik, Astr. och Fysik16, 26 (1922).

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