首页> 美国政府科技报告 >Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

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Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

机译：对于具有52.5度纵横比的后掠翼和直线尾翼的火箭动力模型的升力，阻力和纵向稳定性，在1.4到2.1马赫数下的机翼弧度和扭曲的影响

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Gillespie, Warren, Jr;
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年度 1956
页码 1-30
总页数 30
原文格式 PDF
正文语种 eng
中图分类工业技术;
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3. ACCOUNTING FOR THE ELASTIC TWIST WHEN PROCESSING THE TEST RESULTS FOR THE DRAINED WING MODEL OF HIGH ASPECT RATIO IN A WIND TUNNEL [J] . M.F. Garifullin, O.A. Orlova TsAGI science journal . 2018,第5期

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4. Estimation of the Effect of Lift-drag Ratio caused by Relaxing Longitudinal Static Stability of a certain-type of Joined-Wing Aircraft [C] . Zhen Liang, Weijun Wang International Conference on Mechanical, Electronic, Control and Automation Engineering . 2018

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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. Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4 [O] . Emslie K., Hosking L., Marshall W. S. D. 1953

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Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

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