Investigation of a Technique for Measuring Dynamic Ground Effect in a Subsonic Wind Tunnel PDF Download
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Author:
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Category :
Languages : en
Pages : 68
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Author:
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Category :
Languages : en
Pages : 68
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722318680
Category :
Languages : en
Pages : 40
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A ground-based testing technique is under development for the measurement of dynamic or time-dependent ground effects which may be present during aircraft approach and landing. The technique utilizes a model moving horizontally over an upwardly-inclined ground plane to simulate rate of descent. Results were obtained in the Langley Research Center (LaRC) Vortex Research Facility (VRF) for a generic 60 delta wing and for an F-18 configuration, both with and without thrust reversing, at forward speeds up to 100 ft/sec. These same models and support hardware were also tested in the LaRC 14 by 22 Foot Subsonic Tunnel at identical conditions (but without rate of descent) with and without a moving-belt ground plane to obtain data for comparison. Kemmerly, Guy T. and Paulson, John W., Jr. Langley Research Center RTOP 505-61-71-02...
Author:
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Category : Aeronautics
Languages : en
Pages : 312
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Author: Robert E. Curry
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Category : Airplanes
Languages : en
Pages : 22
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 456
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 380
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ISBN:
Category : Science
Languages : en
Pages : 46
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Category : Government publications
Languages : en
Pages : 1430
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Category : Government publications
Languages : en
Pages : 1388
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Author: Stephen Corda
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Category : Aerodynamics
Languages : en
Pages : 32
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