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Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch

机译：上音调的空气动力特性的掠角和厚度比的作用：在一系列具有为3.5的纵横比和0.2的锥度比弧形翼翼身组合的超音速气动特性

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Driver, Cornelius; Robinson, Ross B;
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年度 1952
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:19:52

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1. A study of high angle of attack aerodynamic characteristics of dalta wing at low speed for development of the next-generation SST [J] . Makoto Kamishita, Shigeru Aso, Yuichi Kumamoto 九州大学工学集報 . 1997,第5期

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2. Effects of wing shape, aspect ratio and deviation angle on aerodynamic performance of flapping wings in hover [J] . Shahzad Aamer, Tian Fang-Bao, Young John, Physics of fluids . 2016,第11期

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3. Component and Vehicle Aerodynamic Characteristics of a Low Aspect Ratio Winged Aerospace Vehicle Configuration [J] . S Chaudhuri, V Shanmugam, J Umakant Journal of the Institution of Engineers (Inida). Aerospace Engineering Division Board . 2006,第Nov期

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4. Investigation into Aerodynamic Characteristics and Flow Structures of Rectangular Flat-plate Wings of Very Small Aspect Ratios at All Angle of Attack [C] . Yusuke NISHIZAKI, Akira URITA, Shuji TANAKA 日本機械学会年次大会 . 2003

机译：在所有攻角中对极小纵横比的矩形平板翼的空气动力学特性和流动结构
5. New acceleration potential method for supersonic unsteady aerodynamics of lifting surfaces, further extension of the nonplanar supersonic doublet point method, and nonlinear, nongradient optimized rational function approximations for supersonic, transient response unsteady aerodynamics. [D] . Tewari, Ashish. 1992

机译：用于提升表面的超音速非稳态空气动力学的新的加速势方法，非平面超音速双重点方法的进一步扩展以及用于超音速，瞬态响应非稳态空气动力学的非线性，非梯度优化有理函数逼近。
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7. 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

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch

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