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

Wong, Thomas J., Gloria, Hermilo R.
naca-rm-a55j07
1955


Results of tests to determine the aerodynamic characteristics of all-movable control and body combinations at angles of attack from 0 degrees to 25 degrees and control deflection angles from -30 degrees to +30 degrees are presented and compared with theory.

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