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Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees

机译：平面和阶梯扰流副翼跨度和展向位置对前缘后掠51.3度机翼横向控制特性影响的研究

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Fischel, Jack; Hammond, Alexander D;
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年度 1950
页码 1-64
总页数 64
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edges [J] . Schuette Andreas Journal of Aircraft . 2017,第2期

机译：圆形前缘后掠翼上涡流的数值研究
2. Effect of Jet Spacing on Swept-Wing Leading-Edge Separation Control [J] . Walker Michael M., Hipp Kyle D., Benton Stuart I, AIAA Journal . 2018,第7期

机译：射流间距对后掠前缘分离控制的影响
3. Numerical Assessment of Leading- and Trailing-Edge Control on a Swept Lambda Wing [J] . Tormalm Magnus, Le Roy Jean-Francois, Morgand Stephane Journal of Aircraft . 2018,第2期

机译：掠过的Lambda机翼前缘和后缘控制的数值评估
4. Numerical study of blunt leading edge separation on a 53 degree swept diamond wing (STO AVT-183) using the Edge and Cobalt flow solvers [C] . Henrik Edefur, Magnus Tormalm, Joe Coppin, AIAA SciTech Forum;AIAA aerospace sciences meeting . 2015

机译：使用Edge和Cobalt流动求解器对53度掠过的钻石机翼（STO AVT-183）进行钝钝前沿分离的数值研究
5. 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。

Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees

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