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Theoretical Characteristics of Two-Dimensional Supersonic Control Surfaces
Report presenting aerodynamic characteristics of uncambered symmetrical parabolic and double-wedge airfoils with leading-edge and trailing-edge flaps using the Busemann second-order-approximation theory. Characteristics presented include aileron effectiveness factor, rate of change of hinge-moment coefficient with aileron deflection, rate of change of the pitching-moment coefficient, and the location of the center of pressure of the airfoil-aileron combination.
Date:
July 27, 1948
Creator:
Morrissette, Robert R. & Oborny, Lester F.
System:
The UNT Digital Library
Investigation of effects of movable exhaust-nozzle plug on operational performance of 20-inch ram jet
Report presenting the effects of a movable exhaust-nozzle plug on the operational performance of a 20-inch ramjet in the altitude wind tunnel. Results were obtained at various exhaust-nozzle-plug positions over a range of fuel-air ratios, combustion-chamber-inlet velocities and static pressures, and ambient-air static pressures.
Date:
July 27, 1948
Creator:
Sterbentz, William H. & Wilcox, Fred A.
System:
The UNT Digital Library