Aerodynamic characteristics of two rectangular-plan-form, all moveable controls in combination with a slender body of revolution at Mach numbers from 3.00 to 6.25
Description:
Report presenting the results of force and moment tests at a range of Mach numbers on two rectangular-plan-form, all-movable controls in combination with a slender body of revolution are presented and compared with the predictions of theory. The results showed that lift variations with angle of attack were somewhat nonlinear for both control-body combinations tested.
Date:
December 28, 1955
Creator:
Wong, Thomas J. & Gloria, Hermilo R.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department