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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an elevon as a longitudinal control and the effects of camber and twist on the maximum lift-drag ratio at supersonic speeds

机译：采用机翼后翼63度的机翼 - 机身组合的空气动力学研究：作为纵向控制的升降机的有效性以及在超音速下弯度和扭曲对最大升力 - 阻力比的影响

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Olson, Robert N; Mead, Merrill H;
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年度 1950
页码 1-55
总页数 55
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Control device effectiveness studies of a 53° swept flying wing configuration. Experimental, computational, and modeling considerations [J] . Loechert Patrick, Huber Kerstin C., Ghoreyshi Mehdi, Aerospace science and technology . 2019,第Octa期

机译：控制设备对53°掠过的机翼构型的有效性研究。
2. Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations [O] . Patrick Löchert, Kerstin C. Huber, Mehdi Ghoreyshi, 2019

机译：控制装置有效性研究53∘扫过飞行翼配置。实验，计算和建模考虑

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an elevon as a longitudinal control and the effects of camber and twist on the maximum lift-drag ratio at supersonic speeds

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