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Investigation of dynamic ground effectAn experimental investigation of dynamic ground effect was conducted in the Univ. of Kansas wind tunnel using delta wings of 60, 70, 75 deg sweep; the XB-70 wing; and the F-104A wing. Both static and dynamic tests were made. Test data were compared to other test data, including dynamic flight test data of the XB-70 and F-104A. Limited flow visualization test were conducted. A significant dynamic effect was found for highly swept delta wings.
Document ID
19870014987
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chang, Ray Chung (Kansas Univ. Lawrence, KS, United States)
Muirhead, Vincent U. (Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Publication Information
Publication: NASA. Ames Research Center Proceedings of the 1985 NASA Ames Research Center's Ground-Effects Workshop
Subject Category
Aerodynamics
Accession Number
87N24420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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