Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane

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论文 Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane 简介
摘要:Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics and drag rise of fighter aircraft 作者 Pierpont, P. K.
关键字 DRAG, FIGHTER AIRCRAFT, LATERAL CONTROL, LATERAL STABILITY, LATERAL STABILITY AND CONTROL, LIFT DRAG RATIO, LONGITUDINAL CONTROL, LONGITUDINAL STABILITY, LONGITUDINAL STABILITY AND CONTROL, STATIC STABILITY, STATIC STABILITY AND CONTROL, TRANSONIC WIND TUNNEL, TRANSONIC WIND TUNNELS, WIND TUNNELS,
类型 Technical Report
来源 NASA,NTRS, 1959/03/01
语言 English(英语)
大小 5929889 Bytes

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