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The Influence of Bypass Turbojet Engine Parameters on the Technical-Economic Characteristics of Long-Range Passenger Aircraft,

机译：旁路涡喷发动机参数对远程客机技术经济性的影响，

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摘要

The report describes parametric study of turbofan engines,intended for subsonic passenger main-liner aircraft with long flight range (up to 15,000km) and increased passenger accommodation (up to 500passengers). As a result of the study it is revealed the optimum values of parameters of operating conditions and the bypass ratio of turbofan engines,providing minimum values of takeoff weight of the aircraft and the smallest operating costs. In the study are also given data on the evaluation of the noise level of contemporary turbofan engines.

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作者
klyachkin, a. l. enenkov, v. g.;
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年度 1974
页码 1-142
总页数 142
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
turbofan engines; performance(engineering); jet transport planes; turbofan enginespassenger aircraft; united states; thermodynamics; lift to drag ratio; fuel systems; costs; jet engine noise; noise reduction; ussr; translations;

机译：涡轮风扇发动机;性能（工程）;喷气式飞机;涡轮风扇发动机客机;美国;热力学;升阻比;燃油系统;成本;喷气发动机噪音;降噪;苏联;翻译;

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1. Research on hypersonic aircraft using pre-cooled turbojet engines [J] . Hideyuki Taguchi, Hiroaki Kobayashi, Takayuki Kojima, Acta astronautica . 2012,第ApraaMay期

机译：使用预冷涡轮喷气发动机的超音速飞机研究
2. Numerical Investigation of the Influence of the Configuration Parameters of a Supersonic Passenger Aircraft on the Intensity of Sonic Boom [J] . V. F. Volkov, I. I. Mazhul’ Journal of engineering physics and thermophysics . 2018,第1期

机译：超音速客机配置参数对Sonic Boom强度影响的数值研究
3. Improving the technical-economic characteristics of aircraft structural elements [J] . M. N. Stepnov, A. N. Lisin, L. N. Morozov, Russian engineering research . 2000,第11期

机译：改善飞机结构元件的技术经济特性
4. MICROTURBO Families of Turbojet Engine for Missiles and Uava??s From the TR60 to the New Bypass Turbojet Engine Generation [C] . J. Rideau, G. Guyader, A. Cloarec AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2008

机译：从TR60到新一代旁路涡轮喷气发动机的导弹和Uava涡轮喷气发动机的MICROTURBO系列
5. The development of turbojet aircraft in Germany, Britain, and the United States: A multi-national comparison of aeronautical engineering, 1935--1946. [D] . Pavelec, Sterling Michael. 2004

机译：1935--1946年，德国，英国和美国的涡轮喷气飞机的发展：多国航空工程比较。
6. The Influence of the Aircraft Operating Fluids on the Mechanical Parameters of the Airport Surface Concrete [O] . Wojciech Żebrowski, Paweł Wolka, Marzena Kurpinska 2020

机译：飞机运行流体对机场混凝土机械参数的影响
7. NUMERICAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF A “WING – FUSELAGE – ENGINE NACELLE – PYLON” THREEDIMENSIONAL LAYOUT OF THE ENGINE FOR A WIDE-BODY LONG-RANGE AIRCRAFT [O] . S.V. Timchenko 2019

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8. The Influence of Errors in Flow Passage Manufacture on the Divergence of Rated Characteristics of Turbojet Engines (Trd) [R] . Tikhonov, A. S., Akhmedzyanov, A. M. 1969

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The Influence of Bypass Turbojet Engine Parameters on the Technical-Economic Characteristics of Long-Range Passenger Aircraft,

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