AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS.
Publication
, Journal Article
Williams, MH; Chi, MR; Ventres, CS; Dowell, EH
Published in: AIAA Journal
1977
A general theory of planar disturbances in inviscid parallel shear flows, analogous to thin-wing theory in potential flows, has been developed. Integral relations between surface pressure and deformation are obtained that are similar to, and can be solved by the same numerical methods as those of potential flow. Computed results are shown that illustrate the effects of a model turbulent boundary layer on various lifting and nonlifting surfaces, including an elastic panel in low supersonic flow and an airfoil control surface in subsonic flow.
Duke Scholars
Published In
AIAA Journal
Publication Date
1977
Volume
15
Issue
8
Start / End Page
1159 / 1166
Related Subject Headings
- Aerospace & Aeronautics
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering
Citation
APA
Chicago
ICMJE
MLA
NLM
Williams, M. H., Chi, M. R., Ventres, C. S., & Dowell, E. H. (1977). AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS. AIAA Journal, 15(8), 1159–1166.
Williams, M. H., M. R. Chi, C. S. Ventres, and E. H. Dowell. “AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS.” AIAA Journal 15, no. 8 (1977): 1159–66.
Williams MH, Chi MR, Ventres CS, Dowell EH. AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS. AIAA Journal. 1977;15(8):1159–66.
Williams, M. H., et al. “AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS.” AIAA Journal, vol. 15, no. 8, 1977, pp. 1159–66.
Williams MH, Chi MR, Ventres CS, Dowell EH. AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS. AIAA Journal. 1977;15(8):1159–1166.
Published In
AIAA Journal
Publication Date
1977
Volume
15
Issue
8
Start / End Page
1159 / 1166
Related Subject Headings
- Aerospace & Aeronautics
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering