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The longitudinal and lateral aerodynamic characteristics at Mach numbers of 1.41 and 2.20 of a variable-sweep fighter model with wing sweeps varying from 25 deg to 75 deg

机译：可变扫描战斗机模型的马赫数为1.41和2.20的纵向和横向空气动力学特性，机翼扫掠从25度到75度不等

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作者
Spearman, M. L.; Harris, R. V., Jr.;
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年度 1963
页码 1-79
总页数 79
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
AERODYNAMIC CHARACTERISTICS; FIGHTER AIRCRAFT; LATERAL STABILITY; LONGITUDINAL STABILITY; VARIABLE SWEEP WINGS; LIFT DRAG RATIO; SUPERSONIC FLOW;

机译：空气动力学特征; FIGHTER aIRCRaFT;横向稳定性;纵向稳定性;可变扫风翼;升降比;超音速流;

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1. Longitudinal Aerodynamic Characteristics of a V/STOL Tilt-wing Four-Propeller Transport Model using a Surface Vorticity Flow Solver [C] . Bryan Sandoz, Vivek Ahuja, Roy Harfield AIAA aerospace sciences meeting;AIAA SciTech forum . 2018

机译：使用表面涡流求解器的V / STOL倾斜翼四螺旋桨运输模型的纵向空气动力学特性
2. Longitudinal and lateral aerodynamic characteristics at Mach numbers from 0.60 to 2.20 of a variable sweep fighter model with wing sweep angles from 25 deg to 75 deg [R] . Spearman, M. L. 1962

机译：机翼扫描角度为25度至75度的可变扫描战斗机模型的马赫数为0.60至2.20的纵向和横向空气动力学特性

The longitudinal and lateral aerodynamic characteristics at Mach numbers of 1.41 and 2.20 of a variable-sweep fighter model with wing sweeps varying from 25 deg to 75 deg

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