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Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane

机译：二面角变化对低纵横比直翼超音速飞机理论动态横向响应特性的影响

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Heinle, Donovan R;
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年度 1950
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Characteristic Properties of Heat Exchange and Gas Dynamics in Supersonic Flow of a Heterogeneous Medium in Micronozzles with a High Aspect Ratio [J] . P. V. NIKITIN, S. M. PROROKOV Heat Transfer Research . 2002,第5a6期

机译：高纵横比微喷嘴中非均相介质超声速流动中的热交换和气体动力学特征
2. Experimental and numerical investigation into the supersonic flow of a weakly ionized plasma around a dihedral angle: Magnetohydrodynamic control of the flow pattern and heat fluxes toward the wall [J] . Bobashev SV, Golovachev YP, Kurbatov GA, Technical physics . 2009,第1期

机译：围绕二面角的弱电离等离子体的超音速流的实验和数值研究：磁流体动力学控制流向和壁的通量
3. Lateral response of cable-guided hoisting system with time-varying length: Theoretical model and dynamics simulation verification [J] . Wang Jinjie, Cao Guohua, Zhu Zhencai, Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science . 2015,第16期

机译：随时间变化的电缆导向提升系统的横向响应：理论模型和动力学仿真验证
4. Study of Changes in the Aerodynamic Characteristics of the Axisymmetric Supersonic Vehicle in Case of Gas Blowing from the Lateral Surface [C] . V. A. Kislovskiy, V. I. Zvegintsev International Conference on the Methods of Aerophysical Research . 2016

机译：侧表面气体吹气时轴对称超音速车辆空气动力学特性的变化研究
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。
6. THE DYNAMIC ANALYSIS OF LOW-ASPECT-RATIO AIRPLANE WINGS [O] . Holt Ashley, Herbert M. Voss, Garabed Zartarian 1954

机译：低纵横比飞机机翼的动力分析
7. THE DYNAMIC ANALYSIS OF LOW-ASPECT-RATIO AIRPLANE WINGS [O] . Ashley, Holt, Voss, Herbert M., Zartarian, Garabed 1954

机译：低纵横比飞机机翼的动力分析

Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane

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