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Effect of wing crank and sweepback on the low subsonic stability and control characteristics of a model of hypersonic boost-glide type airplane

机译：翼型曲柄和后掠对高超声速助推滑翔机模型低亚音速稳定性及控制特性的影响

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作者
Shanks, R. E.;
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年度 1960
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
AIRCRAFT CONTROL; AIRCRAFT STABILITY; BOOSTGLIDE VEHICLES; HYPERSONIC GLIDERS; WIND TUNNEL MODELS; GRAPHS (CHARTS); SUBSONIC SPEED; SWEPTBACK WINGS;

机译：飞机控制;飞机稳定性; BOOsTGLIDE车辆; HYpERsONIC GLIDERs;风洞模型;图表（图表）; sUBsONIC spEED; sWEpTBaCK WINGs;

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专利

1. Computational Modeling of Roughness-Based Laminar Flow Control on a Subsonic Swept Wing [J] . Fei Li, Meelan Choudhari, Chau-Lyan Chang, AIAA Journal . 2011,第3期

机译：亚音速扫掠机翼上基于粗糙度的层流控制的计算模型
2. Robust aeroelastic instability suppression of an advanced wing with model uncertainty in subsonic compressible flow field [J] . Ji-Seok Song, Jeonghwan Choo, Seog-Ju Cha, Aerospace science and technology . 2013,第1期

机译：亚音速可压缩流场中具有模型不确定性的先进机翼的鲁棒气动弹性失稳抑制
3. Modeling the Performance of Hypersonic Boost-Glide Missiles [J] . Cameron L. Tracy, David Wright Science & global security . 2020,第1a3期

机译：造型超声波升压导弹的性能
4. Control of aerodynamic characteristics of airfoils and wing systems in subsonic flow [C] . S. B. Svirschevski, L. G. Artamonova, A. N. Radzig, World Aviation Congress . 2002

机译：亚源流动翼型和翼系统的空气动力学特性控制
5. Turbulence modeling for subsonic separated flows over 2-D airfoils and 3-D wings. [D] . Rosen, Aaron M. 2013

机译：在2D机翼和3D机翼上进行亚音速分离流的湍流建模。
6. On fluttering modes for aircraft wing model in subsonic air flow [O] . Marianna A. Shubov -1

机译：亚音速气流中机翼模型的颤振模式
7. ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating [O] . Tomonori Shimada, Taku Ohwada 2020

机译：从翼前缘发出的三个亚态反流式喷射阵列的ILE，暴露于超声波空气动力学加热
8. Investigation of Low-Subsonic Flight Characteristics of a Model of a Hypersonic Boost-Glide Configuration Having a 78 deg. Delta Wing [R] . Paulson, John W., Shanks, Robert E. 1961

机译：具有78度的高超音速升压 - 滑翔结构模型的低亚音速飞行特性研究。三角洲翼

Effect of wing crank and sweepback on the low subsonic stability and control characteristics of a model of hypersonic boost-glide type airplane

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