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Small-scale transonic investigation of the effects of full-span and partial-leading-edge flaps on the aerodynamic characteristics of a 50 degree 38 foot sweptback wing of aspect ratio 2.98

机译：全尺寸和部分前缘襟翼对纵横比为2.98的50度38英尺后掠翼的空气动力学特性影响的小规模跨音速研究

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Spreeman, Kenneth P; Alford, William J , Jr;
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年度 1952
页码 1-35
总页数 35
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. NONLINEAR AERODYNAMIC EFFECTS ON TRANSONIC FLAP BUZZ, TAIL FLUTTER AND LIMIT-CYCLE OSCILLATIONS OF TWO-DIMENSIONAL WING-FLAP-TAIL CONFIGURATIONS [J] . J.-C. Cheng The Chinese journal of mechanics . 2009,第4期

机译：二维机翼-襟翼-尾翼构造对跨音速襟翼，尾翼颤动和极限周期振动的非线性气动影响
2. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
3. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
4. Experimental investigation of effects of flapping wing aspect ratio and flexibility on aerodynamic performance [C] . Zhang Chengkun, Khan Zaeem A., Agrawal Sunil K. 2010 IEEE International Conference on Robotics and Automation . 2010

机译：襟翼纵横比和柔韧性对空气动力性能影响的实验研究
5. An investigation of the dynamic effects of flap deflection on the aerodynamic characteristics of an airplane wing using computational fluid dynamics [D] . Moerchel, Alexander M. 2006

机译：利用计算流体力学研究襟翼偏转对飞机机翼空气动力学特性的动态影响
6. Some Effects of Taper Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Sweptback Angle of 45° and an Aspect Ratio 4.0 [O] . Eiichi NAKAI, Toshiro TAKAGI, Yasukatsu ANDO 1966

机译：锥形比对一系列薄悬臂机翼的横向振荡特性的一些效果，其具有45°的扫频角和纵横比4.0

Small-scale transonic investigation of the effects of full-span and partial-leading-edge flaps on the aerodynamic characteristics of a 50 degree 38 foot sweptback wing of aspect ratio 2.98

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