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Summary of the Theoretical Lift, Damping-in-Roll, and Center-of-Pressure Characteristics of Various Wing Plan Forms at Supersonic Speeds

机译：理论提升的总结，阻尼式侧倾，以及各种翼计划形式在超音速的中心 - 的 - 压力特性

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摘要

The information for the determination of the theoretical lift, damping-in-roll, and center-of-pressure characteristics for a group of plan forms at supersonic speeds has been collected. This information is presented in three forms: first, equations; second, figures presenting generalized curves in which the quantities plotted are combinations of the geometric and aerodynamic parameters; and third, figures presenting curves for representative groups of specific configurations showing variation of the derivatives with Mach number. From this group several observations have been made as to the effect of taper ratio, angle of sweep, and aspect ratio on the values of the derivatives.

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Piland, R. O.;
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年度 1949
页码 1-5
总页数 5
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Velocity ; Wings ; Supersonic characteristics ; Ratios ; Parameters ; Damping ; Configurations ; Geometry ; Taper ; Mach number ; Equations ; Lift ; Aspect ratio ; Aerodynamics;

机译：速度;翼;超音速特征;比率;参数;阻尼;配置;几何形状;锥度;马赫数;方程;电梯;长宽比;空气动力学;

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机译：在超音速下各种机翼平面形式的理论升力，阻尼 - 滚动和压力中心特征的总结

Summary of the Theoretical Lift, Damping-in-Roll, and Center-of-Pressure Characteristics of Various Wing Plan Forms at Supersonic Speeds

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