An Experimental Investigation of the Ground Vortex Created by a Moving Jet
Author :
Publisher :
Page : 132 pages
File Size : 16,14 MB
Release : 1989
Category :
ISBN :
Experimental Investigation of a Jet Impinging on a Ground Plane in the Presence of a Cross Flow
Author : J. M. Cimbala
Publisher :
Page : 108 pages
File Size : 37,85 MB
Release : 1987
Category : Cross-flow (Aerodynamics).
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Book Description
Scientific and Technical Aerospace Reports
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Publisher :
Page : 702 pages
File Size : 39,32 MB
Release : 1995
Category : Aeronautics
ISBN :
Book Description
The Ground Vortex Flow Field Associated with a Jet in a Cross Flow Impinging on a Ground Plane for Uniform and Annular Turbulent Axisymmetric Jets
Author : William M. Cavage
Publisher :
Page : 172 pages
File Size : 50,58 MB
Release : 1993
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Book Description
NASA SP.
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Page : 706 pages
File Size : 19,41 MB
Release : 1991
Category : Aeronautics
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Book Description
Applied Mechanics Reviews
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Page : 568 pages
File Size : 21,8 MB
Release : 1965
Category : Mechanics, Applied
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Book Description
34th Aerospace Sciences Meeting & Exhibit
Author :
Publisher :
Page : 674 pages
File Size : 46,91 MB
Release : 1996
Category : Aeronautics
ISBN :
Book Description
Aeronautical Engineering
Author :
Publisher :
Page : 538 pages
File Size : 37,20 MB
Release : 1991
Category : Aeronautics
ISBN :
Book Description
Lift and Pitching Moment Induced on Jet STOVL by the Ground Vortex
Author : Vearl R. Stewart
Publisher :
Page : 110 pages
File Size : 32,69 MB
Release : 1993
Category : Ground-cushion phenomenon
ISBN :
Book Description
The data obtained during an investigation of the effects of the ground vortex on a generic wing-body configuration are presented in this report. Circular, rectangular and thrust reverser jets were tested. The tests were conducted in the 14 by 22 foot tunnel at the NASA Langley Research Center. The tests covered a range of heights above the ground, forward velocities, and ground belt speeds.
Lift and Pitching Moment Induced on Jet STOVL Aircraft Hovering in Ground Effect
Author : Richard E. Kuhn
Publisher :
Page : 462 pages
File Size : 45,50 MB
Release : 1993
Category : Ground-cushion phenomenon
ISBN :
Book Description
The data obtained during an investigation of the effects of crossflow on the suckdown and fountain effects induced by various arrangements of vertically impinging jets are presented in this report. The jet arrangements included circular and rectangular jets in various single, dual and triple jet configurations. The tests were conducted in the 14 by 22 foot tunnel at the NASA Langley Research Center. Tests covered a range of heights above the ground, nozzle pressure ratios, and forward velocities.
