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Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2 : two aluminum-alloy models of 20-inch chord with 0.064- and 0.081-inch-thick skin

机译：在马赫数2的自由射流中测试空气动力学加热的多翼机翼结构：两个20英寸和弦的铝合金模型，皮肤厚0.064和0.081英寸

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Griffith, George E; Miltonberger, Georgene H; Rosecrans, Richard;
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年度 1955
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Aerodynamic Modelling and Analysis of a Novel Mechanism for Chord and Camber Morphing Wing [J] . Harun Levent ?ahin, Bora Or?un ?ak?r, Yavuz Yaman MATEC Web of Conferences . 2018,第1期

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3. Aerodynamic Simulation of Low Mach Turbulent Jets with Lattice Boltzmann Models [J] . Yunchong Tu, Shishuai Shishuai Zhang, Junlong Xie, Open Journal of Fluid Dynamics . 2012,第4期

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Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2 : two aluminum-alloy models of 20-inch chord with 0.064- and 0.081-inch-thick skin

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