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Flight investigation from high subsonic to supersonic speeds to determine the zero-lift drag of a transonic research vehicle having wings of 45 degree sweepback, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil sections

机译：从高亚音速到超音速的飞行调查，以确定具有45度后掠翼，纵横比4，锥度比0.6和NaCa 65a006翼型截面的跨音速研究车辆的零升力阻力

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Katz, Ellis;
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年度 1949
页码 1-17
总页数 17
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Distinctive Features of the Flow Past High-Speed Flight Vehicles with Air-Breathing Engines on Subsonic, Transonic, and Low Supersonic Velocity Ranges [J] . N. A. Biagoveshchenskii, V. N. Gusev, S. M. Zadonskii Fluid Dynamics . 2007,第2期

机译：亚音速，跨音速和低超音速速度范围内带有空气呼吸发动机的高速飞行器的气流的显着特征
2. Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections [J] . Thin-Walled Structures . 2019,第Juna期

机译：具有NACA翼型截面的薄壁梁模型的复合材料飞机机翼的自由振动分析
3. Optimization of Airfoils along High-Aspect-Ratio Wing of Long-Endurance Aircraft in Trimmed Flight [J] . Nikolaev Nikolay V Journal of aerospace engineering . 2019,第6期

机译：飞机修整飞行中长航程高比机翼翼型的优化
4. NUMERICAL INVESTIGATION OF THE DRAG OF ROCKETS AT SUBSONIC, TRANSONIC AND SUPERSONIC SPEEDS [C] . Michael Steppert, Philipp Epple ASME international mechanical engineering congress and exposition . 2018

机译：亚音速，超音速和超音速火箭弹的数值研究
5. BASE DRAG EFFECTS ON MAXIMUM LIFT-TO-DRAG RATIO AIRFOILS AT MODERATE SUPERSONIC SPEEDS [D] . PRITCHARD, ROBERT EMLYN -1

机译：在中等超声速下最大升降比比翼型上的基本拉力效应
6. 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

Flight investigation from high subsonic to supersonic speeds to determine the zero-lift drag of a transonic research vehicle having wings of 45 degree sweepback, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil sections

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