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An assessment of ground effects determined by static and dynamic testing techniquesA new testing technique was developed wherein the rate of descent can be included as a parameter in ground effects investigations. This technique simulates the rate of descent by horizontal motion of a model over an inclined ground board in the Langley Vortex Research Facility (VRF) During initial evaluations of the technique, dynamic ground effects data were obtained over the inclined ground board, steady state ground effects data were obtained over a flat portion of the ground board, and the results were compared to conventional static wind tunnel ground effect data both with and without a moving belt ground plane simulation. Initial testing and analysis led to the following conclusions: the moving belt ground plane had little effect on static ground effects for the configurations tested unless thrust reversers were employed; in general, rate-of-descent reduced ground effects to the point that for reversed thrust cases an expected loss of lift due to ground effects was eliminated at approach conditions; and, in general, the steady state results from the VRF matched static results obtained from the wind tunnel once the flow field stabilized over the flat portion of the ground board.
Document ID
19890001483
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Paulson, John W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Kemmerly, Guy T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Publication Information
Publication: NASA, Ames Research Center, The 1987 Ground Vortex Workshop
Subject Category
Aerodynamics
Accession Number
89N10854
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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