Advanced Aircraft Flight Performance: Nomenclature
Advanced Aircraft Flight Performance: Nomenclature
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先进飞机飞行性能：命名法
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发表时间：
2012
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通讯作者：
Antonio Filippone
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作者：
Antonio Filippone
A.菲利彭剑桥大学出版社，爱丁堡大楼，剑桥，CB2 8RU，英国。2012年。635pp。插图。GB 75。ISBN978-1-107-02400-7。这本书阐述了飞机在实际操作环境中的性能，并提出了比概念设计研究中经常使用的封闭解决方案更先进的方法。除了预期的爬升和巡航等飞机性能方面的章节外，后面的章节还涉及寒冷天气、噪音和排放等主题。这本书还考虑了涡扇和涡轮螺旋桨发动机的型号。在这本书的下面是作者编写的一个广泛的软件，在描述如何执行用于分析飞机的许多程序时，参考了这些代码。该规范已被用于提供当前民用飞机的算例结果。这些结果有时被用来讨论高度灵活性等概念，这被认为是将轨迹产生降至最低的一种方法。然而，有时读者会对结果中为什么会出现某些趋势做出自己的结论。有时，这本书的版面似乎与计算机软件过于紧密地结合在一起。早期章节的重要部分是解释飞机是如何被分解成其组成部分的，然后描述如何计算相关的体积和湿面积。这似乎过了头，对于执业工程师来说，这几乎是显而易见的。这本书通常很容易阅读，有清晰的解释，对于第一版来说，印刷错误相对较少。每个方程式的目的都解释得很清楚，尽管有些方程式的起源并不总是很清楚。记法在每一章的末尾都有一个明确的命名法。这本书代表了一个有用的参考经验的性能工程师，它将是一个很好的起点，任何人的任务是执行飞机的性能分析。彼得·伦德，Ceng，MRAES
A. Filippone Cambridge University Press, The Edinburgh Building, Cambridge, CB2 8RU, UK. 2012. 635pp. Illustrated. £75. ISBN 978-1-107-02400-7. This book addresses the performance of aircraft in a real operating environment and it presents methods that are more advanced than the closed solutions frequently used during conceptual design studies. As well as the expected chapters on aspects of aircraft performance such as climb and cruise, later chapters deal with topics such as cold weather, noise and emissions. The book also considers models for turbofan and turboprop engines. Underlying the book is an extensive piece of software written by the author and reference is made to this code when describing how to execute many of the procedures used to analyse an aircraft. This code has been used to provide example results for current civil aircraft. These results are sometimes used to discuss concepts such as altitude flexibility which has been suggested as a way to minimise the generation of contrails. However, sometimes the reader is left to make their own conclusions about why certain trends occur in the results. At times the layout of the book appears to be too closely aligned to the computer software. A significant part of an early chapter is spent explaining how an aircraft is broken down into its constituent parts and then describes how to compute the associated volumes and wetted areas This appears to be excessive and for a practicing engineer, would verge on the obvious. The book is generally easy to read with clear explanations, and for a first edition, there are relatively few typographical errors. The purpose of each equation is clearly explained, although the origin of some equations is not always clear. Notation is clearly defined with a nomenclature at the end of each chapter. The book represents a useful reference for practising performance engineers and it would be a good starting point for anyone tasked with carrying out a performance analysis of an aircraft. Peter Render, CEng, MRAeS