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An Approximate Transonic Calculative Method Applied to Various Smooth Shaped Nose-Cylindrical Bodies.

机译：一种适用于各种光滑型鼻 - 圆柱体的近似跨声力计算方法。

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摘要

An approximate transonic small disturbance technique originally developed for ogival noses and cylindrical afterbodies has been extended to arbitrary smooth nose forebodies and cylindrical afterbodies. Limitations of the method and trends are discussed. (Author)

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作者
venghaus, heinz h. wu,jain-ming;
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年度 1974
页码 1-33
总页数 33
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
projectiles; nose conestransonic flow; cylindrical bodies; ogives; free stream; flow fields; approximation(mathematics);

机译：射弹;鼻内旋转流;圆柱体; ogives;自由流;流场;近似（数学）;
入库时间 2022-08-29 11:40:11

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An Approximate Transonic Calculative Method Applied to Various Smooth Shaped Nose-Cylindrical Bodies.

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