Aircraft Performance

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 22 May 2007

226

Citation

(2007), "Aircraft Performance", Aircraft Engineering and Aerospace Technology, Vol. 79 No. 3. https://doi.org/10.1108/aeat.2007.12779cae.004

Publisher

:

Emerald Group Publishing Limited

Copyright © 2007, Emerald Group Publishing Limited


Aircraft Performance

Aircraft Performance

Maido SaarlasJohn Wiley & Sons LtdUK

Aircraft Performance sets forth a group of tested and proven methods needed to determine the performance of an aircraft. The central theme of this book is the energy method, which enhances understanding of the standard methods and provides accessibility to advanced topics. As a result, readers gain a thorough understanding of the performance issues involved in operating an aircraft in an efficient and economic manner. Intended to be a text book mainly for aeronautical engineering students, this book should also be of value to other engineering students or as reference material to practitioners in the aerospace industry.

While covering all the standard topics – level and climbing flight, range and endurance, take-off and landing, and maneuvering flight – the book focuses on the energy methods applied to path performance analysis. Throughout the text, numerous examples from both the commercial and military sectors show readers how the concepts and calculations are applied to real-life situations. Problems, ranging from basic to complex, test the readers' understanding and provide an opportunity for essential practice.

To help focus the readers' attention on core issues, this text assumes that aerodynamics and propulsion are known inputs. Special appendices are provided to present some aerodynamic and propulsive equations and data. In general, topics are separated into horizontal and vertical plane approaches. Following an introduction and overview, basic energy concepts are employed to obtain a fundamental performance equation.

This text, with its extensive use of examples and problem sets, is ideal for upper-level undergraduate and graduate students in engineering. It also serves as a reference for design engineers in both military and industrial sectors who want a set of clear and reliable methods to calculate aircraft performance.

MaidoSaarlas, who is recently retired, has been a Professor or Chairman of the Aerospace Engineering Department at the US Naval Academy for the last 38 years. He received his undergraduate and master's degrees at the University of Illinois and his doctorate at the University of Cincinnati. His industrial experience includes work with Bell Aircraft, North American, Douglas Aircraft, and General Electric companies. He is an author or co- author of two books: Steam and Gas Turbines for Marine Propulsion and An Introduction to Aerospace Propulsion.

Details available from: John Wiley & Sons Ltd, Tel: +44 (0) 1243 779777; Fax: +44 (0) 1243 775878; web site: www.wiley.com

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