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Design of Airframe-Integrated, Distortion-Tolerant Propulsion Systems.

机译：机身集成，抗扭曲推进系统的设计。

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作者
Florea, R. V.; Hardin, L. W.; Tillman, G.; Shabbir, A.; Sharma, O. P.; Arend, D. J.;
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年度 2011
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Propulsion system configurations; Engine design; Engine airframe integration; Engine inlets; Distortion; Computational fluid dynamics; Blended-wing-body configurations; Boeing aircraft; Propulsive efficiency; Boundary layers; Optimization; Fan blades; Shape optimization;

机译：推进系统配置;发动机设计;发动机机身集成;发动机进气道;失真;计算流体动力学;混合翼体配置;波音飞机;推进效率;边界层;优化;风扇叶片;形状优化;

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1. Performance Evaluation of Airframe-Integrated Aerospike Propulsion Systems in Off-Design Flight Conditions [J] . Hidemi Takahashi Journal of propulsion and power . 2016,第2期

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2. Aerodynamic Database Development for the Hyper-X Airframe-Integrated Scramjet Propulsion Experiments [J] . Walter C. Engelund, Scott D. Holland, Charles E. Cockrell Jr Journal of Spacecraft and Rockets . 2001,第6期

机译：用于Hyper-X机体集成Scramjet推进实验的空气动力学数据库开发
3. Prediction Power Propulsion of the Ship at the Stage of Preliminary Design. Part I: Forecasting Method for Power Propulsion of Ship at the Stage of Preliminary Design [J] . Prof. Tadeusz Szelangiewicz, Dr. Katarzyna ?elazny Management Systems in Production Engineering . 2017,第2期

机译：初步设计阶段的船舶动力预测。第一部分：初步设计阶段船舶动力推进的预测方法
4. Performance Evaluation of Airframe-Integrated Aerospike Propulsion Systems in Off-Design Flight Conditions [C] . Hidemi Takahashi, Takeo Tomita, Sadatake Tomioka AIAA aerospace sciences meeting;AIAA SciTech forum . 2015

机译：在非设计飞行条件下机体集成的气钉推进系统的性能评估
5. Optimal allocation of thermodynamic irreversibility for the integrated design of propulsion and thermal management systems. [D] . Maser, Adam Charles. 2012

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6. Hull and Aerial Holonomic Propulsion System Design for Optimal Underwater Sensor Positioning in Autonomous Surface Vessels [O] . Bruno A. Regina, Leonardo M. Honório, Antônio A. N. Pancoti, 2021

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7. An Experimental Study on Aerodynamic Characteristics of the External Nozzle in Clustered Airframe-Integrated Propulsion System Equipped with the RLV [O] . Tatsushi ISONO, Sadatake TOMIOKA, Noboru SAKURANAKA, 2016

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Design of Airframe-Integrated, Distortion-Tolerant Propulsion Systems.

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