首页> 美国政府科技报告 >TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-l AIRPLANE IN PULL-UPS AT MACH NUMBERS FROM 0.53 TO 0.99

【24h】

TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-l AIRPLANE IN PULL-UPS AT MACH NUMBERS FROM 0.53 TO 0.99

机译：在机械编号从0.53到0.99的下拉式X-1飞机机翼上测量的表面压力系数和气动特性

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

Tabulated pressure coefficients and aerodynamic characteristics are presented for six spanwise stations on the left wing of the Bell X-l research airplane. The data were obtained in 10 pull-ups at Mach numbers from 0.53 to O.99.

著录项

作者
Ronald J. Knapp; Gertrude V. Wilken;
展开▼
作者单位

展开▼
年度 1950
页码 1-79
总页数 79
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
专利

1. Measured aerodynamic coefficients of without and with spiked blunt body at Mach 6 [J] . R. Kalimuthu, R. C. Mehta, E. Rathakrishnan Advances in Aircraft and Spacecraft Science . 2019,第3期

机译：在6马赫速度下不带钝顶体和带尖顶钝体的空气动力学系数
2. Measured aerodynamic coefficients of without and with spiked blunt body at Mach 6 [J] . R. Kalimuthu, R. C. Mehta, E. Rathakrishnan Advances in Aircraft and Spacecraft Science . 2019,第3期

机译：测量的空气动力学系数没有和在马赫6的尖刺钝体
3. Comparison of aerodynamic characteristics provided by wing with bell shaped lift distribution and generalized wings [J] . Pavel Hospodá?, Armand Drábek MATEC Web of Conferences . 2019,第3期

机译：钟形升力分布的机翼和广义机翼提供的空气动力特性比较
4. Aerodynamic Characteristics of a Deployable-Wing Airplane with an Elevon for Mars Exploration [C] . Gouji Yamada, Aya Miyazaki, Hiromitsu Kawazoe Asia-Pacific International Symposium on Aerospace Technology . 2016

机译：展开翼飞机的空气动力学特性，有一个MARS探索
5. An investigation of the dynamic effects of flap deflection on the aerodynamic characteristics of an airplane wing using computational fluid dynamics [D] . Moerchel, Alexander M. 2006

机译：利用计算流体力学研究襟翼偏转对飞机机翼空气动力学特性的动态影响
6. Comparison of aerodynamic characteristics provided by wing with bell shaped lift distribution and generalized wings [O] . Pavel Hospodář, Armand Drábek 2019

机译：机翼与钟形升力分布和广义翼提供的空气动力学特性的比较
7. TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-l AIRPLANE IN AN UNACCELERATED LOW-SPEED STALL, IN PUSHOVERS AT MACH NUMBERS OF 0.83 AND 0.99, AND IN A PULL-UP AT A MACH NUMBER OF 1.16 [R] . Ronald J. Knapp 1951

机译：在机械编号为0.83和0.99的推力器中，在X-1飞机的机翼上测量的压力系数和空气动力学特性，在机械编号为0.83和0.99的推力下，以及在机械机械数为1.16的推力下测量的气动特性和空气动力学特性

TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-l AIRPLANE IN PULL-UPS AT MACH NUMBERS FROM 0.53 TO 0.99

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅