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A review of some Reynolds number effects related to bodies at high angles of attack

机译：回顾一些与大迎角机体有关的雷诺数效应

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摘要

A review of some effects of Reynolds number on selected aerodynamic characteristics of two- and three-dimensional bodies of various cross sections in relation to fuselages at high angles of attack at subsonic and transonic speeds is presented. Emphasis is placed on the Reynolds number ranges above the subcritical and angles of attack where lee side vortex flow or unsteady wake type flows predominate. Lists of references, arranged in subject categories, are presented with emphasis on those which include data over a reasonable Reynolds number range. Selected Reynolds number data representative of various aerodynamic flows around bodies are presented and analyzed and some effects of these flows on fuselage aerodynamic parameters are discussed.

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Polhamus, E. C.;
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年度 1984
页码 1-124
总页数 124
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; CIRCULAR CYLINDERS; MACH NUMBER; REYNOLDS NUMBER; ANGLE OF ATTACK; FLOW DISTRIBUTION; SUPERCRITICAL FLOW; SURFACE ROUGHNESS; VORTEX SHEDDING; WIND TUNNEL TESTS;

机译：空气动力学特征;圆柱;马赫数; REYNOLDs NUmBER;攻击角度;流量分配;超临界流量;表面粗糙度; VORTEX sHEDDING;风洞隧道测试;

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机译：雷诺数效应高攻角
8. Review of Some Reynolds Number Effects Related to Bodies at High Angles of Attack [R] . Polhamus, E. C. 1984

机译：高攻角下与雷诺数相关的雷诺数效应研究综述

A review of some Reynolds number effects related to bodies at high angles of attack

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