首页> 美国政府科技报告 >Application of a double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors

【24h】

Application of a double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors

机译：应用双死区时间模型描述了具有多元件喷射器的液体推进剂火箭发动机的冲击

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

Double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors

著录项

作者
Szuch, J. R.;
展开▼
作者单位

展开▼
年度 1969
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
COMBUSTION STABILITY; INJECTORS; LIQUID PROPELLANT ROCKET ENGINES; MODELS; ANALOG COMPUTERS; HYDROGEN; LIQUID OXYGEN; SWEAT COOLING;

机译：燃烧稳定性; INJECTORs;液体推进剂火箭发动机;楷模;模拟计算机;氢;液体氧气; sWEaT COOLING;

相似文献

外文文献
中文文献
专利

1. Propellant Injector Influence on Liquid-Propellant Rocket Engine Instability [J] . Pavel P. Popov, William A. Sirignano, Athanasios Sideris Journal of propulsion and power . 2015,第1期

机译：推进剂喷油器对液体推进剂火箭发动机不稳定性的影响
2. EXPERIMENTAL INVESTIGATION OF CHARACTERISTICS OF A DOUBLE-BASE SWIRL INJECTOR IN A LIQUID ROCKET PROPELLANT ENGINE [J] . Fathollah OMMI, Koros NEKOFAR, Amir KARGAR, Thermal science . 2010,第2期

机译：液体火箭发动机双基旋流喷枪特性的实验研究
3. Experimental investigation of characteristics of a double-base swirl injector in a liquid rocket propellant engine [J] . Ommi Fathollah, Nekofar Koros, Kargar Amir, Thermal science . 2010,第2期

机译：液体火箭发动机双基涡旋喷油器特性的实验研究
4. Propellant Injector Influence on Liquid Propellant Rocket Engine Instability [C] . Pavel P. Popov, Athanasios Sideris, William A. Sirignano AIAA SciTech forum;Aerospace sciences meeting . 2014

机译：推进剂喷射器对液体推进剂火箭发动机不稳定性的影响
5. Primary atomization study of a swirl coaxial liquid propellant rocket injector. [D] . Rahman, Shamim Aejaz. 1997

机译：涡旋同轴液体推进剂火箭喷射器的初步雾化研究。
6. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970

机译：液体火箭推进剂工作人员的肝脏检查
7. Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [O] . С.С. Гаврюшин, Е.Е. Красновский, О.В. Короткая, 2013

机译：液相推进火箭发动机燃烧室热应力 - 应变评估的副结构方法的应用
8. Application of a Double-Dead-Time Model Describing Chugging to Liquid Propellant Rocket Engines Having Multielement Injectors [R] . Szuch, J. R. 1969

机译：具有多元素喷射器的液体推进剂火箭发动机双死区模型的应用

Application of a double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅