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SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION.

Publication ,  Journal Article
Dowell, EH
Published in: Aeronautical Quarterly
January 1, 1980

Significant new results are presented to show to what extent a simplified theory for transonic flow may be used. Solutions are obtained by classical techniques and compared with experiment. Results are given for two-dimensional and three-dimensional, steady and unsteady flow. The effects of flow separation and improvements in Bernoulli's equation and the surface boundary condition are also briefly discussed.

Duke Scholars

Published In

Aeronautical Quarterly

DOI

ISSN

0001-9259

Publication Date

January 1, 1980

Volume

31

Issue

pt 4

Start / End Page

252 / 284
 

Citation

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Chicago
ICMJE
MLA
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Dowell, E. H. (1980). SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION. Aeronautical Quarterly, 31(pt 4), 252–284. https://doi.org/10.1017/s0001925900008945
Dowell, E. H. “SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION.Aeronautical Quarterly 31, no. pt 4 (January 1, 1980): 252–84. https://doi.org/10.1017/s0001925900008945.
Dowell EH. SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION. Aeronautical Quarterly. 1980 Jan 1;31(pt 4):252–84.
Dowell, E. H. “SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION.Aeronautical Quarterly, vol. 31, no. pt 4, Jan. 1980, pp. 252–84. Scopus, doi:10.1017/s0001925900008945.
Dowell EH. SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION. Aeronautical Quarterly. 1980 Jan 1;31(pt 4):252–284.

Published In

Aeronautical Quarterly

DOI

ISSN

0001-9259

Publication Date

January 1, 1980

Volume

31

Issue

pt 4

Start / End Page

252 / 284