A wind tunnel investigation has been conducted to determine the longitudinal and lateral aerodynamic characteristics of a model of a supersonic cruise fighter configuration with a design Mach number of 2.60. The configuration is characterized by a highly swept arrow wing twisted and cambered to minimize supersonic drag due to lift, twin wing mounted vertical tails, and an aft mounted integral underslung duel-engine pod. The investigation also included tests of the configuration with larger outboard vertical tails and with small nose strakes.
Subsonic and Supersonic Aerodynamic Characteristics of a Supersonic Cruise Fighter Model with a Twisted and Cambered Wing with 74 Deg Sweep
1977
63 pages
Report
Keine Angabe
Englisch