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Low-amplitude damping-in-pitch characteristics of tailless delta-wing-body combinations at Mach numbers from 0.80 to 1.35 as obtained with rocket-powered models

机译：用火箭动力模型得到的马赫数为0.80到1.35的无尾三角翼组合的低幅度阻尼 - 俯仰阻尼特性

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D'Aiutolo, Charles T;
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年度 1954
页码 1-36
总页数 36
原文格式 PDF
正文语种 eng
中图分类工业技术;
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机译：两种机构线性组合建模的10马赫弓形冲击非定常模型
6. Direct numerical simulation of homogeneous turbulence in combination with premixed combustion at low Mach number modelled by the $G$-equation [O] . T. C. TREURNIET, F. T. M. NIEUWSTADT, B. J. BOERSMA 2006

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Low-amplitude damping-in-pitch characteristics of tailless delta-wing-body combinations at Mach numbers from 0.80 to 1.35 as obtained with rocket-powered models

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