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Empirical Formulas for the Prediction of the Base Pressure of Missile Bodies at Subsonic Velocities

机译：亚音速下导弹体基压预测的经验公式

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摘要

Formulas for predicting base pressure of missile bodies at incidence are provided. The formulas are valid for cylindrical and boattailed afterbodies at free stream subsonic Mach numbers up to 0.9.

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作者
Tanner, M.;
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年度 1985
页码 p.1-47
总页数 47
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Base pressure; Missile bodies; Subsonic speed; Afterbodies; Boattails; Cylindrical bodies;

机译：基础压力;导弹体;亚音速;后体;船尾;圆柱体;

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8. Theoretical Prediction of Base Pressure on Missile Bodies Having a Turbulent Dead-Air Region at Supersonic Velocities [R] . Tanner, M. 1981

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Empirical Formulas for the Prediction of the Base Pressure of Missile Bodies at Subsonic Velocities

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