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
APA
Chicago
ICMJE
MLA
NLM
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