THE STATIC AERODYNAMIC CHARACTERISTICS OF A VARIABLE SWEEP WING RESEARCH MODEL.
DAVID TAYLOR MODEL BASIN WASHINGTON D C AERODYNAMICS LAB
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A wind tunnel study was conducted to determine the effect of Mach number, angle of attack, and wing sweep angle on the longitudinal aerodynamic characteristics of a variable sweep wing research model. The study was conducted at Mach numbers between 0.60 and 1.15 and at angles of attack from -2 to 16 degrees. The report presents the data for the static phase of the investigation. Author
- Fluid Mechanics