Variable thickness shear layer aerodynamics revisited
Publication
, Journal Article
Dowell, EH; Chi, MR
Published in: AIAA J. (USA)
1977
For shear layers of slowly varying thickness it is shown that it is sufficient to replace the constant boundary-layer thickness used in the kernel function by Ventres (1975) in the analysis of lifting surfaces, by the varying thickness. (This kernel function relates pressure on the lifting surface to the normal velocity on its surface). The results of the approach compare favourably in terms of accuracy and calculation length with the results of previous approaches
Duke Scholars
Published In
AIAA J. (USA)
Publication Date
1977
Volume
15
Issue
5
Start / End Page
745 / 747
Related Subject Headings
- Aerospace & Aeronautics
- 4012 Fluid mechanics and thermal engineering
- 4001 Aerospace engineering
- 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 revisited. AIAA J. (USA), 15(5), 745–747.
Dowell, E. H., and M. R. Chi. “Variable thickness shear layer aerodynamics revisited.” AIAA J. (USA) 15, no. 5 (1977): 745–47.
Dowell EH, Chi MR. Variable thickness shear layer aerodynamics revisited. AIAA J (USA). 1977;15(5):745–7.
Dowell, E. H., and M. R. Chi. “Variable thickness shear layer aerodynamics revisited.” AIAA J. (USA), vol. 15, no. 5, 1977, pp. 745–47.
Dowell EH, Chi MR. Variable thickness shear layer aerodynamics revisited. AIAA J (USA). 1977;15(5):745–747.
Published In
AIAA J. (USA)
Publication Date
1977
Volume
15
Issue
5
Start / End Page
745 / 747
Related Subject Headings
- Aerospace & Aeronautics
- 4012 Fluid mechanics and thermal engineering
- 4001 Aerospace engineering
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering