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Author : Virgil E. Johnson
Publisher :
Page : 84 pages
File Size : 27,44 MB
Release : 1961
Category : Cavitation
ISBN :
Author : Virgil E. Johnson
Publisher :
Page : 104 pages
File Size : 29,44 MB
Release : 1957
Category : Aerodynamics
ISBN :
Abstract: The existing two-dimensional theory for the characteristics of supercavitating hydrofoils operating at zero cavitation number is modified to include the effects of camber, aspect ratio, and depth of submersion. For a comparison with the theory, two aspect-ratio-1 hydrofoils, a flat plate and one with a cambered lower surface, were tested by operating them near the water surface so that their upper surfaces were completely ventilated. The data obtained verified the theory to within 3 percent. Some experimental data are also presented for the models operating at nonzero cavitation number for both air and water-vapor-filled cavities.
Author : Virgil E. Johnson
Publisher :
Page : 0 pages
File Size : 17,95 MB
Release : 1957
Category : Cavitation
ISBN :
Theoretical expressions for the lift, drag, and center of pressure of super-cavitating hydrofoils of arbitrary section, aspect ratio, and depth of submersion are developed for the zero-cavitation-number case.
Author :
Publisher :
Page : 88 pages
File Size : 12,35 MB
Release : 1961
Category :
ISBN :
Author :
Publisher :
Page : 78 pages
File Size : 29,12 MB
Release : 1961
Category : Cavitation
ISBN :
Author : Langley Aeronautical Laboratory
Publisher : Hassell Street Press
Page : 104 pages
File Size : 43,34 MB
Release : 2021-09-09
Category :
ISBN : 9781013793417
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Author : Kenneth W. Christopher
Publisher :
Page : 36 pages
File Size : 10,14 MB
Release : 1960
Category : Hydrofoils
ISBN :
Author : Ken W. Christopher
Publisher :
Page : 56 pages
File Size : 28,81 MB
Release : 1960
Category : Hydrodynamics
ISBN :
Author : Kenneth W. Christopher
Publisher :
Page : 60 pages
File Size : 19,27 MB
Release : 1960
Category :
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 448 pages
File Size : 33,81 MB
Release : 1960
Category : Aeronautics
ISBN :