Experimentally Determined Effects of Varying Pitch and Control Stiffnesses on the Flutter Characteristics at Supersonic Speeds of All-movable Wing and Tail Models

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论文 Experimentally Determined Effects of Varying Pitch and Control Stiffnesses on the Flutter Characteristics at Supersonic Speeds of All-movable Wing and Tail Models 简介
摘要:Pitch and control stiffness effects on flutter characteristics of all-moveable wing and vertical and horizontal tails on fighter aircraft at supersonic speeds 作者 Hanson, P. W.
关键字 AIRSPEED, FIGHTER AIRCRAFT, FLUTTER, FLUTTER ANALYSIS, HORIZONTAL TAIL, HORIZONTAL TAIL SURFACES, STABILIZERS (FLUID DYNAMICS), STIFFNESS, SUPERSONIC SPEED, TAIL ASSEMBLIES, VERTICAL TAIL, WINGS,
类型 Technical Report
来源 NASA,NTRS, 1959/03/01
语言 English(英语)
大小 1716598 Bytes

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Experimentally Determined Effects of Varying Pitch and Control Stiffnesses on the Flutter Characteristics at Supersonic Speeds of All-movable Wing and Tail Models 相关资料