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The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel

机译：在Langley 20英尺自由旋转隧道中的旋转平衡上测量的旋转姿态的1/10比例模型的战斗机飞机的气动力和力矩

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作者
Stone, Ralph W , Jr; Burk, Sanger M , Jr; Bihrle, William, Jr;
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年度 1950
页码 1-61
总页数 61
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
RUDDER CONTROLS; SPINNING - RECOVERY; SPINNING CHARACTERISTICS - EFFECT OF WING FLAPS; SPINNING CHARACTERISTICS - EFFECT OF LANDING GEARS; SPINNING CHARACTERISTICS - EFFECT OF TAIL SURFACES; ROLLING, PITCHING & YAWING MOMENTS; WIND TUNNEL TESTS - NACA - FREE-SPINNING (20 FEET); SPINNING TESTS, WIND-TUNNEL; MANEUVERABILITY - FIGHTERS;

机译：舵控制;纺纱 - 恢复;纺纱特性 - 翼片的效果;纺纱特性 - 起落架的影响;纺纱特性 - 尾部表面的影响; ROLLING，pITCHING＆amp; YaWING mOmENTs;风洞隧道测试 - NaCa - 自由旋转（20英尺）;纺纱试验，风洞;可操作性 - 战士;

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1. INVESTIGATION OF ROTARY AND UNSTEADY DERIVATIVES OF THE PITCHING MOMENT OF AN AIRPLANE MODEL USING A 2DOF FORCED OSCILLATION RIG [J] . I. V. Kolin, K. F. Latsoev, V. G. Markov, TsAGI science journal . 2013,第4期

机译：利用2自由度强迫振动台研究飞机模型俯仰矩的旋转和非稳态导数。
2. An accelerometer balance for aerodynamic force measurements over Hypervelocity Ballistic models in shock tunnel [J] . Balakalyani Gomathinayagam, Jagadeesh Gopalan Measurement . 2019,第期

机译：气动力测量对震动隧道超高速弹道模型的气动力测量加速度计平衡
3. Aerodynamic force measurement using 3-component accelerometer force balance system in a hypersonic shock tunnel [J] . S. Saravanan, G. Jagadeesh, K. P. J. Reddy Shock Waves . 2009,第6期

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4. Wind Tunnel Rig for the Study of Roll Damping and Pitch Damping Effects of Free-Spinning Models at Supersonic Speed [C] . Leopold F., Gastebois G., Lacour A., Instrumentation in Aerospace Simulation Facilities, 2005. iciasf '05. 21st International Congress on . 2005

机译：风洞钻机研究超音速自由旋转模型的侧倾阻尼和节距阻尼效应
5. A Force Balance Model of Early Spindle Pole Separation in Drosophila Embryos [O] . E. N. Cytrynbaum, J. M. Scholey, A. Mogilner 2003

机译：果蝇胚胎早期纺锤极分离的力平衡模型。
6. Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes [O] . Bowman James S. Jr., Hultberg Randy S., Martin Colin A. 1989

机译：在自旋姿态下旋转运动期间飞机模型的尾部和后部机身压力的测量
7. Aerodynamic Forces and Moments on a 1/10-Scale Model of a Fighter Airplane in Spinning Attitudes as Measured on a Rotary Balance in the Langley 20-Foot Free-Spinning Tunnel [R] . Stone, R. W., Burk, S. M., Bihrle, W. J. 1950

机译：气动力和气动纺纱态度上的战斗机飞机的1/10比例模型时刻，在兰利20英尺自由旋转的隧道测量在旋转平衡

The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel

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