首页> 美国政府科技报告 >Preliminary Investigation of Performance of a Wedge Nozzle Applicable to a Supersonic Cruise Aircraft

【24h】

Preliminary Investigation of Performance of a Wedge Nozzle Applicable to a Supersonic Cruise Aircraft

机译：适用于超音速巡航飞机的楔形喷嘴性能初探

获取原文

页面导航

著录项
引文网络
相似文献
相关主题

著录项

作者
Jeracki, R. J.; Johns, A. L.;
展开▼
作者单位

展开▼
年度 1971
页码 1-3
总页数 3
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Nozzle flow ; Nozzle geometry ; Wedge flow ; Gas flow ; Nozzle efficiency ; Performance tests ; Supersonic jet flow;

机译：喷嘴流动;喷嘴几何形状;楔形流动;气体流动;喷嘴效率;性能测试;超音速射流;

相似文献

外文文献
中文文献
专利

1. EXPERIMENTAL INVESTIGATION OF THE NOZZLES OF SUBSONIC AND SUPERSONIC AIRCRAFT [J] . G. N. Lavrukhin, V. A. Talyzin TsAGI science journal . 2014,第8期

机译：亚音速和超音速飞机喷嘴的实验研究
2. NUMERICAL INVESTIGATION OF ELLIPTICAL MIXED EXPANSION NOZZLE PERFORMANCE IN SUPERSONIC FLOW [J] . Anatoliy Pavlovich Mazurov TsAGI science journal . 2019,第1期

机译：超声速流动中椭圆混合扩展喷嘴性能的数值研究
3. Numerical Investigation of the Effects of Primary Nozzle Diverging Portion on Performance of the Supersonic Ejector of an Ejector Refrigeration Cycle [J] . Shaban Alyari Shourehdeli, Kamran Mobini, Ali Asakereh International journal of air-conditioning and refrigeration . 2019,第3期

机译：一次喷嘴扩散部分对喷射器制冷循环超音速喷射器性能影响的数值研究
4. AERODYNAMIC DESIGN OF SINGLE-EXPANSIONRAMP NOZZLE FOR AIRCRAFT WITH SUPERSONIC CRUISE SPEED OF FLIGHT [C] . A.V. Shenkin, A.P. Mazurov, A.P. Bykov Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：飞行器超音速飞行器单膨胀进气口气动设计
5. Wind tunnel testing of a supersonic cruise nozzle in subsonic ejector configuration. [D] . Jones, Jesse Thomas. 2009

机译：亚音速喷射器配置中的超音速巡航喷嘴的风洞测试。
6. Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows [O] . X. Gao, G. X. Xiang, W. J. Tang, -1

机译：超音速流中双扫/双斜坡楔引起的复流研究
7. An experimental investigation on the performance of conical nozzles for argon cluster formation in supersonic jets [O] . Haiyang Lu, Guoquan Ni, Ruxin Li and Zhizhan Xu 2010

机译：超声速射流中锥形喷嘴形成氩团簇性能的实验研究
8. Preliminary investigation of performance of a wedge nozzle applicable to a supersonic cruise aircraft [R] . Jeracki, R. J., Johns, A. L. 1971

机译：适用于超音速巡航飞机的楔形喷嘴性能的初步研究

Preliminary Investigation of Performance of a Wedge Nozzle Applicable to a Supersonic Cruise Aircraft

著录项

引文网络

相似文献

相关主题

期刊订阅