首页> 美国政府科技报告 >Force and pressure-recovery characteristics of a conical-type nose inlet operating at Mach numbers of 1.6 to 2.0 and at angles of attack to 9 degrees

【24h】

Force and pressure-recovery characteristics of a conical-type nose inlet operating at Mach numbers of 1.6 to 2.0 and at angles of attack to 9 degrees

机译：锥形鼻入口的力和压力恢复特性，马赫数为1.6至2.0，攻角为9度

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
Beke, Andrew; Allen, J L;
展开▼
作者单位

展开▼
年度 1952
页码 1-22
总页数 22
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. Investigation of the Magnus Effect of a Generic Projectile at Mach 3 Up to 16 Degrees Angle of Attack [J] . D. Klatt, R. Hruschka, F. Leopold Journal of Applied Mechanics: Transactions of the ASME . 2013 ,第3期

机译：普通弹丸在3马赫至16度迎角范围内的马格努斯效应研究
2. An analytical model for airfoil aerodynamic characteristics over the entire 360 degrees angle of attack range [J] . International journal of applied mechanics . 2020 ,第3期

机译：整个360度攻击范围内翼型空气动力学特性的分析模型
3. Analysis and Design of a Scramjet Engine Inlet Operating from Mach 5 to Mach 10 [J] . Luu Hong Quan, Nguyen Phu Hung, Le Doan Quang, International Journal of Mechanical Engineering and Applications . 2016 ,第1期

机译：从5马赫到10马赫的Scramjet发动机进气道的分析和设计
4. INVESTIGATION OF THE MAGNUS EFFECT ON A GENERIC PROJECTILE AT MACH 3 UP TO 16 DEGREES ANGLE OF ATTACK [C] . D. Klatt, R. Hruschka, F. Leopold International symposium on ballistics . 2013

机译：在高达16度攻角的Mach 3上通用射弹的马格努球效应调查
5. Hypersonic boundary-layer transition measurements at Mach 10 on a large seven-degree cone at angle of attack [D] . Moraru, Ciprian G. 2015

机译：在大七度锥面的迎角处以10马赫的高超声速边界层跃迁测量
6. Practice Characteristics of Bachelor of Science and Doctor of Pharmacy Degreed Pharmacists Based on the 2009 National Workforce Survey [O] . David H. Kreling, William R. Doucette, Elizabeth H. Chang, 2010

机译：基于2009年国家劳动力调查的理学学士学位和药学博士学位的实践经验
7. Two-dimensional cascade tests of MCA blades in the high transonic Mach number region. 2nd report, On the effect of stagger angle on inlet Mach number characteristics. [O] . Hajime SAKAGUCHI, Susumu TAKAMORI 1990

机译：高跨音机马赫数区域的MCA叶片的二维级联试验。第2次报告，关于入口马赫数特征的错开角度。

Force and pressure-recovery characteristics of a conical-type nose inlet operating at Mach numbers of 1.6 to 2.0 and at angles of attack to 9 degrees

摘要

著录项

相似文献

相关主题

期刊订阅