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Damping in roll of rocket-powered test vehicles having swept, tapered wings of low aspect ratio

机译：在具有低纵横比的扫掠，锥形机翼的火箭动力测试车辆的阻尼中阻尼

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Sanders, E Claude; Edmondson, James L;
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年度 1951
页码 1-27
总页数 27
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number [J] . Wei Zhaoyu, New T. H., Lian Lian, Ocean Engineering . 2019,第JUNa1期

机译：前缘结节在非常低的雷诺数下延迟了锥形后掠式机翼的气流分离
2. Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number [J] . Wei Zhaoyu, New T. H., Lian Lian, Ocean Engineering . 2019,第Juna1期

机译：前沿结节在非常低的雷诺数下锥形扫反翼延迟流分离
3. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
4. Investigation of Eddy Viscosity Turbulence Models on the Vortical Flow over the Highly Swept and Low Aspect Ratio Wing [C] . Keisuke Ohira, Michele Gaffuri, Dongyoun Kwak, AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2013

机译：高掠掠低长宽比机翼涡流的涡流湍流模型研究
5. A model for roll stall and the inherent stability modes of low aspect ratio wings at low Reynolds numbers. [D] . Shields, Matt. 2014

机译：低雷诺数下的低失速比机翼侧倾失速和固有稳定性模式的模型。
6. Modeling and Closed Loop Flight Testing of a Fixed Wing Micro Air Vehicle [O] . Harikumar Kandath, Jinraj V. Pushpangathan, Titas Bera, 2018

机译：固定翼微型飞行器的建模和闭环飞行测试
7. An experimental investigation of the aerodynamic characteristics of a low aspect ratio swept wing with blowing in a spanwise direction from the tips. [O] . Ayers R. F., Wilde M. R. 1956

机译：从尖端向翼展方向吹扫的低纵横比后掠翼的空气动力学特性的实验研究。

Damping in roll of rocket-powered test vehicles having swept, tapered wings of low aspect ratio

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