首页> 美国政府科技报告 >The effect of sweepback on the longitudinal characteristics at a Mach number of 1.24 of a 1/30 scale semispan model of the Bell X-5 airplane from tests by the NACA wing flow method

【24h】

The effect of sweepback on the longitudinal characteristics at a Mach number of 1.24 of a 1/30 scale semispan model of the Bell X-5 airplane from tests by the NACA wing flow method

机译：通过NaCa机翼流动方法的试验，回扫对贝尔X-5飞机的1/30比例半飞机模型的马赫数1.24的纵向特性的影响

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Morris, Garland J; Kennedy, Robert M; Silsby, Norman S;
展开▼
作者单位

展开▼
年度 1950
页码 1-23
总页数 23
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
中文文献
专利

1. Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel [J] . Thi Tuyet Nhung Le, Thanh Phat Duong, Nhat Truong Hoang International Journal of Transportation Engineering and Technology . 2016,第4a1期

机译：低速风洞中NACA0012机翼模型制造气动弹性基准试验的方法
2. A priori tests of subgrid-scale models in an anisothermal turbulent channel flow at low mach number [J] . Dupuy Dorian, Toutant Adrien, Bataille Francoise International Journal of Thermal Sciences . 2019,第期

机译：低马赫数在一个阴道湍流通道流中的子级模型的先验测试
3. Determination of Magnetic Characteristics of Alternative Current Electrotechnical Devices Using the Method of Full-Scale-Model Tests [J] . A.M. Lankin, M.V. Lankin, V.V. Grechikhin, Research Journal of Applied Sciences: RJAS . 2015,第10期

机译：全面模型测试方法确定交流电子设备的磁特性
4. Longitudinal Aerodynamic Characteristics of a V/STOL Tilt-wing Four-Propeller Transport Model using a Surface Vorticity Flow Solver [C] . Bryan Sandoz, Vivek Ahuja, Roy Harfield AIAA aerospace sciences meeting;AIAA SciTech forum . 2018

机译：使用表面涡流求解器的V / STOL倾斜翼四螺旋桨运输模型的纵向空气动力学特性
5. Comparison of data correction methods for blockage effects in semispan wing model testing [O] . Anwar U Haque, Waqar Asrar, Ashraf A Omar, 2016

机译：半柱翼模型测试中堵塞效果的数据校正方法的比较

The effect of sweepback on the longitudinal characteristics at a Mach number of 1.24 of a 1/30 scale semispan model of the Bell X-5 airplane from tests by the NACA wing flow method

摘要

著录项

相似文献

相关主题

期刊订阅