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Longitudinal stability characteristics at transonic speeds of a canard configuration having a 45 degree sweptback wing of aspect ratio 6.0 and NACA 65A009 airfoil section

机译：具有纵横比为6.0的后掠翼和NaCa 65a009翼型截面的鸭式构造的跨音速的纵向稳定性特征

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Vitale, A James; Mcfall, John C , Jr;
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年度 1954
页码 1-26
总页数 26
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
2. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
3. Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations [J] . G. Q. Zhang, S. C. M. Yu, A. Chien, Journal of Aircraft . 2013,第2期

机译：卡纳德前掠机翼构型的空气动力学特性
4. Effect of trailing edge serration on the lift and drag characteristics of NACA0012 airfoil wing [C] . Usama Hussain, Saif Ul Malook, Burhan Shabir, AIAA applied aerodynamics conference;AIAA Aviation Forum . 2017

机译：后缘锯齿对NACA0012机翼机翼升力和阻力特性的影响
5. Some Effects of Taper Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Sweptback Angle of 45° and an Aspect Ratio 4.0 [O] . Eiichi NAKAI, Toshiro TAKAGI, Yasukatsu ANDO 1966

机译：锥形比对一系列薄悬臂机翼的横向振荡特性的一些效果，其具有45°的扫频角和纵横比4.0

Longitudinal stability characteristics at transonic speeds of a canard configuration having a 45 degree sweptback wing of aspect ratio 6.0 and NACA 65A009 airfoil section

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