首页> 外文会议>AIAA Aviation Technology, Integration and Operations Conference >Simplified Thrust and SFC Calculations of Modern Two- Shaft Turbofan Engines for Preliminary Aircraft Design

【24h】

Simplified Thrust and SFC Calculations of Modern Two- Shaft Turbofan Engines for Preliminary Aircraft Design

机译：用于初步飞机设计的现代两轴涡发发动机的简化推力和SFC计算

获取原文

页面导航

著录项
相似文献
相关主题

著录项

来源
《AIAA Aviation Technology, Integration and Operations Conference》|2007年||共15页
会议地点
作者

展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类航空;
关键词

相似文献

外文文献
中文文献
专利

1. Simplified Thrust and Fuel Consumption Models for Modern Two-Shaft Turbofan Engines [J] . Matthias Bartel, Trevor M. Young Journal of Aircraft . 2008,第4期

机译：现代两轴涡扇发动机的简化推力和油耗模型
2. Thrust Performance Evaluation of a Turbofan Engine Based on Exergetic Approach and Thrust Management in Aircraft [J] . Yalcin Enver International Journal of Turbo and Jet Engines . 2017,第2期

机译：基于防辐射方法的涡轮机发动机推力绩效评价与飞机推力管理
3. Review of Thrust Reverser Mechanism used in Turbofan Jet Engine Aircraft [J] . Mohd Anees Siddiqui, Md Shakibul Haq International journal of instrumentation science and engineering . 2013,第1期

机译：涡扇喷气发动机飞机推力反向器机构综述
4. Simplified Thrust and SFC Calculations of Modern Two- Shaft Turbofan Engines for Preliminary Aircraft Design [C] . M. Bartel, T. Young AIAA Aviation Technology, Integration and Operations Conference;ATIO . 2007

机译：用于飞机初步设计的现代两轴涡扇发动机的简化推力和SFC计算
5. The development and testing of an in-flight thrust determination method for a Pratt & Whitney JT15D-1 turbofan engine. [D] . Sanders, Thomas Wayne. 1993

机译：普惠JT15D-1涡扇发动机空中推力确定方法的开发和测试。
6. Fault Diagnostics for Turbo-Shaft Engine Sensors Based on a Simplified On-Board Model [O] . Feng Lu, Jinquan Huang, Yaodong Xing 2012

机译：基于简化的车载模型的涡轮轴发动机传感器故障诊断
7. Thrust Reverser for a Separate Exhaust High Bypass Ratio Turbofan Engine and its Effect on Aircraft and Engine Performance [O] . Tashfeen Mahmood, Anthony Jackson, Vishal Sethi, 2015

机译：用于单独排气高旁通比涡扇发动机的推力换向器及其对飞机和发动机性能的影响
8. EVALUATION OF A SIMPLIFIED GROSS THRUST CALCULATION TECHNIQUE USING TWO PROTOTYPE F100 TURBOFAN ENGINES IN AN ALTITUDE FACILITY [R] . Frank J. Kurtenbach 1979

机译：在高原设施中使用两种原型F100 TURBOFaN发动机评估简化的推力计算技术

获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

客服微信
服务号