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The evaluation of matrix elements for the analysis of swept-back wing structures by the method of oblique coordinates

机译：斜坐标法评估后掠式机翼结构的矩阵元素评估

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摘要

This report is an addition to the college of Aeronautic Report No. 31. The purpose of the report is to enable one to obtain the matrix elements used in the analysis of swept-back wing structures by oblique coordinated in a very rapid manner.

机译：该报告是航空学院31号报告的补充。该报告的目的是使人们能够以非常快速的方式通过倾斜协调来获得用于分析后掠式机翼结构的矩阵元素。

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Lewis S. R.;
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年度 1951
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原文格式 PDF
正文语种 {"code":"en","name":"English","id":9}
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专利

1. Beam-propagation method for analysis of z-dependent structures that uses a local oblique coordinate system [J] . Chiou YP., Chang HC. Optics Letters . 1998,第13期

机译：使用局部倾斜坐标系的z依赖结构的光束传播方法
2. Fast Evaluation of Matrix Elements in Time-Domain Integral Equation Analysis of Planar Structures [J] . M. Khosravi-Farsani, S. Hossein Hesamedin Sadeghi, R. Moini IEEE Transactions on Electromagnetic Compatibility . 2016,第2期

机译：平面结构时域积分方程分析中矩阵元素的快速评估
3. A sampling point quadrature method for 3-node triangular element for the evaluation of element stiffness matrix in finite element analysis [J] . Shyjo Johnson, T. Jeyapoovan, D. Nagarajan International Journal of Computational Materials Science and Engineering . 2020,第2期

机译：三节点三角形元素对有限元分析中元素刚度矩阵评价的采样点正交方法
4. Asymptotic method for evaluating matrix elements in microstrip antenna analysis [C] . Choon Sae Lee, Tung-Hung Hsieh . 1995

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5. Analysis of the effects of vein arrangements on insect wing structure with Finite Element Method [D] . Wang, Yijun. 2016

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6. Comparison and evaluation of stresses generated by rapid maxillary expansion and the implant-supported rapid maxillary expansion on the craniofacial structures using finite element method of stress analysis [O] . Varun Jain, Tarulatha R. Shyagali, Prabhuraj Kambalyal, 2017

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7. On the application of oblique coordinates to problems of plane elasticity and swept-back wing structures [O] . Hemp W. S. 1950

机译：关于斜坐标在平面弹性和后掠机翼结构问题中的应用
8. THE EVALUATION OF MATRIX ELEMENTS FOR THE ANALYSIS OF SWEPT-BACK WING STRUCTURES BY THE METHOD OF OBLIQUE CO-ORDINATES [R] . S. R. LEWIS 1951

机译：后掠机翼结构的矩阵元为分析的通过倾斜坐标的方法进行的评价

The evaluation of matrix elements for the analysis of swept-back wing structures by the method of oblique coordinates

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