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The effects of high-lift devices on the low-speed stability of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow

机译：高扬程装置对直线和滚动流动中纵横比3的锥形37.5度后掠翼的低速稳定性的影响

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Contains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow.

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作者
Queijo, M J; Lichtenstein, Jacob H;
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年度 1948
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
SWEEP - COMPLETE WINGS; FLAPS - COMPLETE WINGS; SLOTS AND SLATS - COMPLETE WINGS; STABILITY, LATERAL - STATIC; STABILITY, DIRECTIONAL - STATIC; DAMPING DERIVATIVES - STABILITY;

机译：sWEEp - 完整的翅膀;襟翼 - 完整的翅膀;插槽和插座 - 完整的机翼;稳定性，横向 - 静态;稳定性，方向性 - 静态;阻尼衍生物 - 稳定性;

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1. On the physics and kinematics of vortex motion in the downstream of a high aspect ratio wing with high-lift devices [J] . A. Das, G. Wichmann Aerospace science and technology . 2004,第6期

机译：具有高升力装置的高长宽比机翼下游涡流运动的物理和运动学
2. Low-Speed Aerodynamic Characteristics of Supercritical Airfoil with Small High-Lift Devices from Flow Pattern Measurements [J] . Thai Duong Nguyen, Masashi Kashitani, Masato Taguchi Journal of Flow Control, Measurement & Visualization . 2020,第4期

机译：流量模式测量小型高升力装置的超临界翼型的低速空气动力学特性
3. Low-Speed Aerodynamic Characteristics of Supercritical Airfoil with Small High-Lift Devices from Flow Pattern Measurements [J] . Thai Duong Nguyen, Masashi Kashitani, Masato Taguchi 流量控制、测量及可视化（英文） . 2020,第004期

机译：流量模式测量小型高升力装置的超临界翼型的低速空气动力学特性
4. NUMERICAL AND EXPERIMENTAL STUDY OF A FLOW OVER STRAIGHT AND SWEPT HIGH-LIFT WINGS [C] . Rumyantsev Andrey, Silantyev Vladimir Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：直形高弯机翼流动的数值与实验研究
5. Jet noise of high aspect-ratio rectangular nozzles with application to pneumatic high-lift devices. [D] . Munro, Scott Edward. 2002

机译：高纵横比矩形喷嘴的喷射噪声应用于气动高升力设备。
6. Effects side effects and plasma concentrations of terbutaline in adult asthmatics after inhaling from a dry powder inhaler device at different inhalation flows and volumes. [O] . T Engel, B Scharling, B Skovsted, 1992

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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

The effects of high-lift devices on the low-speed stability of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow

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