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An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : static longitudinal stability and control characteristics at a Mach number of 1.59

机译：对超音速飞机配置的研究，其具有圆弧形截面和40度后掠的锥形机翼：静态纵向稳定性和马赫数为1.59的控制特性

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Spearman, M Leroy; Hilton, John H , Jr;
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年度 1950
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Investigation on improving longitudinal static stability of a blended wing body aircraft [J] . Zhongyang Qi, Siyu Zong, Yankui Wang CEAS Aeronautical Journal . 2021,第4期

机译：改善混纺机翼体飞机纵向稳定性的调查
2. EXPERIMENTAL INVESTIGATION OF THE SUPERSONIC BOUNDARY LAYER STABILITY ON A SWEPT WING AT MACH NUMBER M = 2 [J] . Yu. G. Ermolaev, A. D. Kosinov, N.V. Semionov TsAGI science journal . 2011,第1期

机译：马赫数为M = 2的掠过翼上超音速边界层稳定性的实验研究
3. Study on longitudinal stability improvement of flying wing aircraft based on synthetic jet flow control [J] . Xu Xiaoping, Zhou Zhou Aerospace science and technology . 2015,第OCTaaNOVa期

机译：基于合成射流控制的机翼纵向稳定性改进研究
4. Numerical Approach Aspects for the Investigation of the Longitudinal Static Stability of a Transport Aircraft with Circulation Control [C] . Dennis Keller STAB/DGLR Symposium . 2014

机译：具有循环控制的运输飞机纵向稳定性的数值接近方面
5. Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers) [O] . Campion B. S. 1954

机译：估计畸变对高速后掠机翼纵向稳定性的影响（亚临界马赫数）

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : static longitudinal stability and control characteristics at a Mach number of 1.59

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