High-Speed Wind-Tunnel Tests of a Twin-Fuselage Pursuit Airplane
Description:
Report discussing the aerodynamic characteristics of a twin-fuselage pursuit airplane model, especially at high speeds. Information about the force data and critical Mach numbers for parts of the model is provided. Suggestions for increasing the Mach number of divergence by making modifications to the wing-fuselage fillets and external shape of the radiator are also included.
Date:
April 24, 1946
Creator:
Anderson, Joseph L. & Tkac, Victor B.
Partner:
UNT Libraries Government Documents Department