Variable thickness shear layer aerodynamics revis ited.
Publication
, Journal Article
Dowell, EH; Chi, MR
Published in: AIAA Journal
1977
The author points out that for shear layers of slowly varying thickness it is sufficient to replace the constant boundary layer thickness which appears in Ventres' Kernal function (AIAA J.,13 Sep. 1975 pp.1183-1189) by the varying thickness. The Kernal function in question is that relating pressure on the lifting surface to its downwash (normal velocity on its surface).
Duke Scholars
Published In
AIAA Journal
Publication Date
1977
Volume
15
Issue
5 ,May 1977
Start / End Page
745 / 747
Related Subject Headings
- Aerospace & Aeronautics
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering
Citation
APA
Chicago
ICMJE
MLA
NLM
Dowell, E. H., & Chi, M. R. (1977). Variable thickness shear layer aerodynamics revis ited. AIAA Journal, 15(5 ,May 1977), 745–747.
Dowell, E. H., and M. R. Chi. “Variable thickness shear layer aerodynamics revis ited.” AIAA Journal 15, no. 5 ,May 1977 (1977): 745–47.
Dowell EH, Chi MR. Variable thickness shear layer aerodynamics revis ited. AIAA Journal. 1977;15(5 ,May 1977):745–7.
Dowell, E. H., and M. R. Chi. “Variable thickness shear layer aerodynamics revis ited.” AIAA Journal, vol. 15, no. 5 ,May 1977, 1977, pp. 745–47.
Dowell EH, Chi MR. Variable thickness shear layer aerodynamics revis ited. AIAA Journal. 1977;15(5 ,May 1977):745–747.
Published In
AIAA Journal
Publication Date
1977
Volume
15
Issue
5 ,May 1977
Start / End Page
745 / 747
Related Subject Headings
- Aerospace & Aeronautics
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering