Zur Theorie der ebenen, instationären Unterschallströmung um ein schwingendes Profil im Kanal-Reference-Cited by-同舟云学术

Zur Theorie der ebenen, instationären Unterschallströmung um ein schwingendes Profil im Kanal

Published:1965-11 Issue:6 Volume:16 Page:770-780
ISSN:0044-2275
Container-title:Zeitschrift für angewandte Mathematik und Physik ZAMP
language:de
Short-container-title:Journal of Applied Mathematics and Physics (ZAMP)

Author:

Meister Erhard

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/BF01614104.pdf

Reference8 articles.

1. R. L. Bisplinghoff, H. Ashley undR. L. Halfman,Aeroelasticity (Addison-Wesley Publ. Comp., Cambridge, Mass. 1955).

2. H. L. Runyan undCh. E. Watkins,Considerations on the Effect of Wind-tunnel Walls on Oscillating Air Forces for Two-dimensional Subsonic Compressible Flow, N.A.C.A. Rep. No. 1150 (1953).

3. H. L. Runyan, D. S. Woolston undA. G. Rainey,Theoretical and Experimental Investigations of the Effect of Tunnel Walls on the Forces on an Oscillating Airfoil in Two-dimensional Subsonic Compressible Flow, N.A.C.A. Rep. No. 1262 (1956).

4. W. P. Jones,Wind-tunnel Wall Interference Effects on Oscillating Aerofoils in Subsonic, Rep. Memor. Aeron. Res. Council, London, No. 2943 (1953).

5. J. W. Miles,The Compressible Flow Past an Oscillating Airfoil in a Wind-tunnel, J. aeron. Sci.23, 671 (1956).

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