Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities

机译：来自不同脉冲设施的10马赫超燃冲压发动机测量结果的比较

获取原文

获取原文并翻译 | 示例

页面导航

著录项
相似文献
相关主题

著录项

来源
《16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference》|2009年|1-8|共8页
会议地点 Bremen(DE)
作者
M. McGilvray; R. Kirchhartz; T. Jazra;
展开▼
作者单位

University of Queensland, St Lucia, Australia;

University of Queensland, St Lucia, Australia;

University of Queensland, St Lucia, Australia;

展开▼
会议组织
原文格式 PDF
正文语种 eng
中图分类各类型航空器;
关键词

相似文献

外文文献
中文文献
专利

1. Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities [J] . Matthew McGilvray Rainer Kirchhartzand Thomas Jazra AIAA Journal . 2010,第8期

机译：来自不同脉冲设施的10马赫超燃冲压发动机测量结果的比较
2. Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities [J] . Matthew McGilvray, Rainer Kirchhartz, Thomas Jazra AIAA Journal . 2010,第8期

机译：来自不同脉冲设施的10马赫超燃冲压发动机测量结果的比较
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. Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities [C] . M. McGilvray, R. Kirchhartz, T. Jazra American Institute of Aeronautics and Astronautics/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference . 2009

机译：Mach 10 Scramjet测量的比较来自不同的冲动设施
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. A Comparison of Delayed Self-Heterodyne Interference Measurement of Laser Linewidth Using Mach-Zehnder and Michelson Interferometers [O] . Albert Canagasabey, Andrew Michie, John Canning, 2011

机译：使用Mach-Zehnder和Michelson干涉仪对激光线宽延迟自外差干涉测量的比较
7. Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility [O] . Paull, A., Stalker, R. J., Mee, D. J. 1993

机译：脉冲设备中完整轴对称超燃冲压发动机的推力测量
8. 1998 Calibration of the Mach 4.7 and Mach 6 Arc-Heated Scramjet Test Facility Nozzles [R] . Witte, David W., Irby, Richard G., Auslender, Aaron H., 2004

机译：1998年mach 4.7和mach 6电弧加热超燃冲压发动机测试设备喷嘴的校准

Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities

著录项

相似文献

相关主题

期刊订阅