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Aerothermodynamics and Jet Propulsion最新文献

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Thermodynamic Properties of Stoichiometric Combustion Products 化学计量燃烧产物的热力学性质
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.018
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引用次数: 0
Chemical Rocket Performance 化学火箭性能
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.015
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引用次数: 0
Viscous Boundary Layer and Thermal Boundary Layer 粘性边界层和热边界层
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.007
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引用次数: 0
Thermodynamics of Air-Breathing Engines 吸气式发动机热力学
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.010
1. Define propulsion efficiency. 2. Define thermal efficiency. 3. Define engine overall efficiency. 4. Define propeller efficiency. 5. Define thrust specific fuel consumption (TSFC). 6. Define brake specific fuel consumption (BSFC). 7. What is the Brayton cycle and which are the two parameters that define it? 8. What is the expression of the thrust of a turbojet? 9. How does the thrust and the thrust specific fuel consumption of a turbojet engine vary with altitude? Justify your answer. Hint: consider that inlet diffuser efficiency, compressor efficiency, turbine efficiency do not vary with altitude. 10. Explain why T SF C turbojet > T SF C turbof an. 11. Draw the real cycle of a turbofan and explain the processes that take place in the engine. 12. Define bypass ratio (BPR). Which value of the BPR is better: 1 or 5? Justify your answer. 13. Which thrust value of a turbofan engine is larger: takeoff thrust or thrust at cruise velocity? Justify your answer. 14. What are the means of generating thrust with a turboprop engine? 15. Why is the use of the turboprop engines limited to airplanes flying at M=0.5 or less? 16. Define static equivalent shaft horsepower (ESHP). Explain why it is necessary to use ESHP? 17. What is the type of the jet engine shown in the figure? Mark on the figure the name and location of as many components as possible. Briefly describe the role of each component. 18. An engineer who works in your jet-engine design team produced this real-cycle h-s diagram. How many mistakes can you find in the diagram? Explain them.
1. 确定推进效率。2. 定义热效率。3.确定发动机的整体效率。4. 定义螺旋桨效率。5. 定义推力比燃料消耗(TSFC)。6. 定义制动比油耗(BSFC)。7. 什么是布雷顿循环定义它的两个参数是什么?8. 涡轮喷气发动机推力的表达式是什么?9. 涡轮喷气发动机的推力和推力比油耗如何随高度变化?证明你的答案。提示:考虑进口扩散器效率,压缩机效率,涡轮效率不随海拔变化。10. 解释为什么tsf - C涡喷发动机> tsf - C涡喷发动机。11. 画一个真实的涡轮风扇的循环,并解释在发动机中发生的过程。12. 定义旁路比(BPR)。BPR的哪个值更好:1还是5?证明你的答案。13. 涡扇发动机哪个推力值更大:起飞推力还是巡航速度推力?证明你的答案。14. 涡轮螺旋桨发动机产生推力的方法是什么?15. 为什么涡轮螺旋桨发动机的使用仅限于以M=0.5或更低的速度飞行的飞机?16. 定义静态等效轴马力(ESHP)。解释为什么必须使用ESHP?17. 图中所示的喷气发动机是什么类型的?在图上标出尽可能多的部件的名称和位置。简要描述每个组件的作用。18. 一位在你的喷气发动机设计团队工作的工程师制作了这个真实循环的h-s图。你能在图表中找出多少错误?解释它们。
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引用次数: 0
Jet Engine Components 喷气发动机部件
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.011
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引用次数: 0
Jet Propulsion Principle 喷气推进原理
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.004
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引用次数: 0
Thermodynamic Properties Tables for Air 空气热力学性质表
Pub Date : 2021-12-02 DOI: 10.1017/9781108691055.017
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引用次数: 0
Air-Breathing Engines 吸气式引擎
Pub Date : 2010-02-17 DOI: 10.1017/9781108691055.009
Zoeb Husain
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引用次数: 1
Introduction to Combustion 燃烧概论
Pub Date : 1995-10-19 DOI: 10.1201/b17027-6
S. Turns
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引用次数: 430
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Aerothermodynamics and Jet Propulsion
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