NASA NTRS · 19870017425
An experimental investigation of dynamic ground effect
Abstract
Experimental studies were conducted to determine the longitudinal force and moment aerodynamic coefficients for a 1/48 scale model of an F-106 aircraft and a 0.01 scale model of an XB-70-1 aircraft. The two airplanes and one 60 degree delta wing model were designed and fabricated to satisfy the specific test conditions of the Kansas University wind tunnel with a 3 by 4.3 test section. Results of the tests are given
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Lee, Pai Hung, Lan, C. Edward, Muirhead, Vincent U.. 1986-04-01. An experimental investigation of dynamic ground effect. https://ntrs.nasa.gov/citations/19870017425
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