NASA-TN-D-30 : Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplane
سازمان: NASA - National Aeronautics and Space Administration (NASA)
کلید واژه: AERODYNAMIC CHARACTERISTICS , AERODYNAMIC COEFFICIENTS , AERODYNAMIC CONFIGURATIONS , AERODYNAMIC DRAG , C-135 AIRCRAFT , FLIGHT TESTS , JET AIRCRAFT , LIFT , MACH NUMBER , MANEUVERS , SUBSONIC SPEED , SWEPT WINGS
سال: 1960
زبان: English
قیمت: 55000 تومان
The lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering flight over the Mach number range from 0.70 to 0.85 for the airplane in the clean configuration at an altitude of 26,000 feet. Data were also obtained over the speed range of 130 knots to 160 knots at 9,000 feet for various flap deflections with gear down.