NASA NTRS · 19870014987
Investigation of dynamic ground effect
Abstract
An 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.
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Chang, Ray Chung, Muirhead, Vincent U.. 1987-02-01. Investigation of dynamic ground effect. https://ntrs.nasa.gov/citations/19870014987
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