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A Novel and Simple Model for Preliminary Aircraft Parameters Selection Using Turbofan Engine Database

机译：涡粉发动机数据库初步飞机参数选择的新颖简单模型

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Aircraft engine selection is an important part of both the design process of a new aircraft and the re-powering of an existing aircraft. This paper is a step further on Svoboda's turbofan engine database as a preliminary design tool, aiming at a novel and simple tool for turbofan engine selection during the preliminary aircraft parameters definition as well as at evaluating current configurations and identifying future trends for the turbofan engines.

机译：飞机发动机选择是新飞机设计过程的重要组成部分和现有飞机的重新供电。本文是SVOBODA的涡波船发动机数据库进一步作为初步设计工具的一步，旨在在初步飞机参数定义期间进行涡扇发动机选择的新颖和简单的工具，以及评估当前配置并识别涡扇发动机的未来趋势。

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《SAE Brazil Congress and Exhibit》|2006年||共13页
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作者
Ricardo Pereira das Neves; Alexandre Osti Fraccaroli; Joao Roberto Barbosa;
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原文格式 PDF
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中图分类 U46-53;
关键词
Databases; Exhaust emissions; Turbofan engines; Weight;

机译：数据库;废气排放;涡扇发动机;重量;

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专利

1. Turbofan engine database as a preliminary design tool [J] . Charlie Svoboda Aircraft Design . 2000,第1期

机译：涡轮风扇发动机数据库作为初步设计工具
2. Modeling Geared Turbofan and Open Rotor Engine Performance for Year-2050 Long-Range and Short-Range Aircraft [J] . Francesco S. Mastropierro, Joshua Sebastiampillai, Florian Jacob, Journal of Engineering for Gas Turbines and Power . 2020,第4期

机译：为2050年远程和短程飞机的齿轮传动涡轮风扇和开式转子发动机性能建模
3. Exergy modeling for evaluating sustainability level of a high by-pass turbofan engine used on commercial aircrafts [J] . Balli Ozgur Applied thermal engineering: Design, processes, equipment, economics . 2017,第期

机译：用于评估商用飞机的高旁路涡扇发动机可持续性水平的高度建模
4. A Novel and Simple Model for Preliminary Aircraft Parameters Selection Using Turbofan Engine Database [C] . Ricardo Pereira das Neves, Alexandre Osti Fraccaroli, Joao Roberto Barbosa SAE Brazil Congress and Exhibit . 2006

机译：涡粉发动机数据库初步飞机参数选择的新颖简单模型
5. Experimental study of a simple thrust model for a Pratt and Whitney JT15D-1 turbofan engine. [D] . Ramsey, Matthew Nelson. 1993

机译：普惠JT15D-1涡扇发动机简单推力模型的实验研究。
6. Aircraft Engine Prognostics Based on Informative Sensor Selection and Adaptive Degradation Modeling with Functional Principal Component Analysis [O] . Bin Zhang, Kai Zheng, Qingqing Huang, 2020

机译：基于信息传感器选择和功能主成分分析的自适应退化建模的飞机发动机预测
7. Modelling Geared Turbofan and Open Rotor Engine Performance for Year-2050 Long-Range and Short-Range Aircraft [O] . Joshua Sebastiampillai, Florian Jacob, Francesco S. Mastropierro, 2019

机译：涡轮涡轮机造型和年2050年远程和短距离飞机的开放式转子发动机性能
8. Preliminary study of optimum ductburning turbofan engine cycle design parameters for supersonic cruising [R] . Fishbach, L. H. 1978

机译：超音速巡航最佳燃烧涡扇发动机循环设计参数的初步研究

A Novel and Simple Model for Preliminary Aircraft Parameters Selection Using Turbofan Engine Database

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