首页> 美国政府科技报告 >Method for Calculating Wing Characteristics by Lifting-Line Theory Using Nonlinear Section Lift Data

【24h】

Method for Calculating Wing Characteristics by Lifting-Line Theory Using Nonlinear Section Lift Data

机译：方法通过提升线理论的非线性部分提升数据计算荣特点

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Material from various sources is combined with some original work into the method of calculating wing characteristics by lifting-line theory. Multhopp's systems of multipliers are employed to obtain the induced angle of attack directly from the spanwise lift distribution. Detailed examples are given for symmetrical lift distribution. Wing characteristics calculated from general nonlinear lift data have been found to agree much closer with experimental data in the region of maximum lift than those calculated on the consumption of linear section lift curves.

著录项

作者
Sivells, J. C.; Neely, R. H.;
展开▼
作者单位

展开▼
年度 1947
页码 1-50
总页数 50
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Wings ; Angle of attack ; Aerodynamic lift ; Experimental data ; Nonlinear analysis;

机译：翅膀迎角;气动升力;实验数据;非线性分析;

相似文献

外文文献
中文文献
专利

1. Stall Recovery of a Morphing Wing via Extended Nonlinear Lifting-Line Theory [J] . Gamble Lawren L., Pankonien Alexander M., Inman Daniel J. AIAA Journal . 2017,第9期

机译：扩展非线性提升线理论的变形翼失速恢复
2. Prediction of Lift Coefficient for Tandem Wing Configuration or Multiple-Lifting-Surface System Using Prandtl’s Lifting-Line Theory [J] . Hao Cheng, Hua Wang International journal of aerospace engineering . 2018,第1期

机译：基于Prandtl的升力线理论的串联机翼构型或多升降面系统升力系数预测
3. Prediction of Lift Coefficient for Tandem Wing Configuration or Multiple-Lifting-Surface System Using Prandtl's Lifting-Line Theory [J] . Cheng Hao, Wang Hua International journal of aerospace engineering . 2018,第PTa2期

机译：基于Prandtl的升力线理论预测串联机翼构型或多起升地面系统的升力系数
4. Predicting Maximum Lift Coefficient for Twisted Wings Using Lifting-Line Theory [C] . W. F. Phillips, N. R. Alley AIAA Aerospace Sciences Meeting . 2007

机译：使用升降线理论预测扭曲翼的最大提升系数
5. A General Approach to Lifting-line Theory, Applied to Wings with Sweep [D] . Reid, Jackson T. 2020

机译：升降线理论的一般方法，应用于扫掠的翅膀
6. Calculating the Mean Amplitude of Glycemic Excursions from Continuous Glucose Data Using an Open-Code Programmable Algorithm Based on the Integer Nonlinear Method [O] . Xuefei Yu, Liangzhuo Lin, Jie Shen, 2018

机译：使用基于整数非线性方法的开放代码可编程算法从连续葡萄糖数据中计算血糖波动的平均幅度
7. Prediction of Lift Coefficient for Tandem Wing Configuration or Multiple-Lifting-Surface System Using Prandtl’s Lifting-Line Theory [O] . Hao Cheng, Hua Wang 2018

机译：使用Prandtl升降线理论预测串联翼配置或多重升降表面系统的提升系数
8. Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data [R] . Sivells, James C, Neely, Robert H 1947

机译：用非线性截面升力数据提升线理论计算机翼特性的方法

Method for Calculating Wing Characteristics by Lifting-Line Theory Using Nonlinear Section Lift Data

摘要

著录项

相似文献

相关主题

期刊订阅