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原文请求
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题 名：
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Location of Detailed Shock Wave in Front of a Body Moving at Supersonic Speed
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并列题名：
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作 者：
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Laitone, E. V.; Pardee, O. O.
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作者机构：
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National Aeronautics and Space Administration, Moffett Field, CA. Ames Research Center.
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团体作者：
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摘 要：
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It is shown that for velocities slightly in excess of sonic, the position of detached shock wave located in front of a given body at zero angle of attack may be estimated theoretically to a reasonable degree of accuracy. In case of bodies of revolution the result was simple, but for two-dimensional bodies, pressure coefficient varies with Mach number, and slight difficulty appears. Theory developed compares favorably with available experimental data.
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分 类 号：
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关 键 词：
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Shock waves ;Supersonic characteristics
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出 版 年：
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报 告 号：
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NACA-RM-A7B10
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ISBN：
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NULL
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ISSN：
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NULL
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页 码：
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1-28
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页 数：
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语 种：
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eng
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馆 藏 号：
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NTIS-ADA800635
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