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Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness

机译：有限厚度矩形翼上恒弦部分跨控制面超声速流动的理论特征

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作者
Tucker, Warren A; Nelson, Robert L;
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年度 1948
页码 1-24
总页数 24
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CONTROL SURFACES - CHARACTERISTICS; WINGS, RECTANGULAR; THEORIES - FLOW SUPERSONIC; THEORIES - FLOW - BUSEMANN; THEORIES - FLOW LINEAR; CONTROL SURFACES - EFFECT OF COMPRESSIBILITY; CONTROL SURFACES - HINGE MOMENTS;

机译：控制表面 - 特征; WINGs，RECTaNGULaR;理论 - 流量超人;理论 - 流动 - 布斯曼;理论 - 流线型;控制表面 - 可压缩性的影响;控制表面 - HINGE mOmENTs;

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1. Nonlinear aeroelastic analysis of a two-dimensional wing with control surface in supersonic flow [J] . Guoyong Zheng 力学学报：英文版 . 2010,第003期

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2. Nonlinear aeroelastic analysis of a two-dimensional wing with control surface in supersonic flow [J] . Guoyong Zheng 力学学报：英文版 . 2010,第003期

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3. Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing [J] . HiroshiYamashita, NaoshiKuratani, MasahitoYonezawa, International journal of aerospace engineering . 2013,第4期

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5. A numerical study of the effect of frequency of pulsed flow control applied to a rectangular cavity in supersonic crossflow. [D] . Stanek, Michael J. 2005

机译：超声速横流中矩形腔上脉冲流控制频率影响的数值研究。
6. Numerical Laser Energy Deposition on Supersonic Cavity Flow and Sensor Placement Strategies to Control the Flow [O] . Ibrahim Yilmaz, Selin Aradag 2013

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7. Numerical calculation of flow fields about rectangular wings of finite thickness in supersonic flow [O] . Vogel, Jerald Milo 1973

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Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness

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