1. Calculation of Initial Vortex Roll-Up in Aircraft Wakes
- Author
-
John E. Yates
- Subjects
Leading edge ,Fuselage ,business.industry ,Incompressible flow ,Separation (aeronautics) ,Aerospace Engineering ,Dynamic pressure ,Aerodynamics ,Aerospace engineering ,business ,Geology ,Vortex ,Added mass - Abstract
Melzig, H. D., "The Dynamic Pressure Loading on Parachute Canopies," AIAA Aerodynamic Deceleration Systems Conference, AIAA, Houston, Texas, 1966. Poppleton, E. D., private communication, Univ. of Sydney, Sydney, Australia. Karmacheti, Principles of Ideal Fluid Aerodynamics, Wiley, New York, 1966. Wood, R. D., "Pressure Distributions on Parachutes During Inflation," Ph.D. thesis, Univ. of Sydney, 1970. Brown, C. E. and Michael, W. H., "On Slender Wings with Leading Edge Separation," TN 3430,1955, NACA. Ibrahim, S. K., "Apparent Added Mass and Moment of Inertia of Cup-Shaped Bodies in Unsteady Incompressible Flow," Ph.D. thesis, University of Minnesota, 1965. more...
- Published
- 1974
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