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A method of selecting the thickness, hollowness, and size of a supersonic wing for least drag and sufficient bending strength at specified flight conditions

机译：一种选择超音速机翼的厚度，空心度和尺寸的方法，用于在特定飞行条件下的最小阻力和足够的弯曲强度

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作者
Amick, James L;
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年度 1952
页码 1-43
总页数 43
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
WINGS; WINGS, COMPLETE - DESIGN VARIABLES;

机译：WINGs; WINGs，COmpLETE - 设计变量;

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专利

1. Supersonic Wing-Body Two-Level Wave Drag Optimization Using Extended Far-Field Composite-Element Methodology [J] . Xiaohui Guan AIAA Journal . 2014,第5期

机译：使用扩展远场复合元素方法的超音速机翼两级波阻力优化
2. Supersonic wing-body wave drag co-ordinated optimisation based on FCE methodology [J] . X. Guan The Aeronautical Journal . 2014,第1209期

机译：基于FCE方法的超音速机翼波阻力协调优化
3. New Supersonic Wing Far-Field Composite-Element Wave-Drag Optimization Method [J] . Brenda Kulfan Journal of Aircraft . 2009,第5期

机译：超音速机翼远场复合元件波阻优化新方法
4. AERODYNAMIC DESIGN OF THREE-DIMENSIONAL BIPLANE WINGS FOR LOW WAVE-DRAG SUPERSONIC FLIGHT [C] . Daigo MARUYAMA Congress of the International Council of the Aeronautical Sciences;ICAS 2008 . 2008

机译：低波拖曳超音速飞行的二维双翼机翼气动设计
5. A wing design methodology for low-boom low-drag supersonic business jet. [D] . Le, Daniel B. 2009

机译：用于低动量低阻力超音速公务机的机翼设计方法。
6. Flight State Identification of a Self-Sensing Wing via an Improved Feature Selection Method and Machine Learning Approaches [O] . Xi Chen, Fotis Kopsaftopoulos, Qi Wu, 2018

机译：通过改进的特征选择方法和机器学习方法识别自感翼的飞行状态
7. Influence of Heat-Treatment on the Adhesive Strength between a Micro-Sized Bonded Component and a Silicon Substrate under Bend and Shear Loading Conditions [O] . Chiemi Ishiyama 2012

机译：热处理对弯曲和剪切负载条件下微尺寸键合组分和硅衬底之间的粘合强度的影响
8. Method of Selecting the Thickness, Hollowness, and Size of a Supersonic Wing for Least Drag and Sufficient Bending Strength at Specified Flight Conditions [R] . Amick, J. L. 1952

机译：在特定飞行条件下选择超音速和足够弯曲强度的超音速翼的厚度，空心度和尺寸的方法

A method of selecting the thickness, hollowness, and size of a supersonic wing for least drag and sufficient bending strength at specified flight conditions

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