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Theory of Flight (Dover Books on Aeronautical Engineering), by Richard von Mises
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"An outstanding textbook." — Scientific, Medical and Technical Books
Almost unsurpassed as a balanced, well-written account of fundamental fluid dynamics, Theory of Flight may still be recommended for a clearer presentation than is to be forced in many more recent works, though it is limited to situations in which air compressibility effects are unimportant.
Designed for the college senior or beginning graduate student, the text assumes a knowledge of the principles of calculus and some training in general mechanics. It is unusual in offering a well-balanced introduction, stressing equally theory and practice. It avoids the formidable mathematical structure of fluid dynamics, while conveying by often unorthodox methods a full understanding of the physical phenomena and mathematical concepts of aeronautical engineering. Theory of Flight contains perhaps the best introduction to the general theory of stability, while the introduction to dynamics of incompressible fluids and the chapters on wing theory remain particularly valuable for their clarity of exposition and originality of thought.
Mises' position as one of the great pioneers in the development of the aeronautical sciences lends a flavor of authenticity not found in more conventional textbooks. Any student who has made himself familiar with his exposition of the fundamentals and applications will have acquired an excellent background for additional, more specialized fields of modern aeronautical engineering.
- Sales Rank: #699180 in eBooks
- Published on: 2012-04-27
- Released on: 2012-04-27
- Format: Kindle eBook
Most helpful customer reviews
48 of 49 people found the following review helpful.
Theory of Flight: The Fundamentals of Aeronautical Design
By Herb Ziegler
To say the text is a classic work on the subject is an understatement. It offers a lucid introduction to the many concepts of aeronautical design that traditionally challenge students. It is a required text for those wishing to advance their understanding of theoretical aerodynamics and its profound implications toward applied aircraft design. Though prerequisite knowledge of aeronautics will augment the text, none is assumed by the author and the mathematical derivations presented within are complete. Most of the empirical data and equations are still quite valid although the text was printed decades ago, before aerodynamics attained its current level of analysis. Anyone involved in the development of subsonic conventional aircraft will want to add this to their research library as a valuable reference.
37 of 37 people found the following review helpful.
Great comprehensive intro to aeronautical engineering
By calvinnme
This book is unlike any on its subject I have ever encountered. Even though the author of this book passed away in 1953, it has a clearness and depth directed towards understanding the essentials of flight that make it a worthwhile - and very inexpensive - read today. Of course, to supplement this book, given the progress made in the field since the author's death, you'll require several textbooks.
Part one is entitled "Equilibrium and Steady Flow in the Atmosphere". Chapter one of that section, though correct in its physics, is simply not applicable to high-speed or turbine-powered aircraft. The other chapters in part one, though, are a great introduction to the dynamics of incompressible fluids that are still completely relevant.
Part two is entitled "The Airplane Wing", and contains material that the author not only expertly compiled, he actually contributed much of this material to wing theory himself. Again, you'll need supplementary material to be current on this information.
Part three is entitled "Propeller and Engine". Where propellers are still in use, the information in this book is correct. The basics on the airplane engine are here, but again time has marched on as to the forefront of technology.
Part four on "Airplane Performance" talks about performance problems in propeller planes. You'll need other material to understand how the jet engine affects performance.
Part five on "Airplane Control and Stability" contains great sections on the theory of non-uniform flight and also a very clear introduction to the theory of dynamic stability. Information on automatic controls is missing, though.
I'd say read this book and use it as a reference as a basis for understanding the mathematics and theory of flight. Use it as a firm foundation for learning about the more modern aspects of the field. One thing I really appreciated about this book is how it is essentially self-contained. The author develops the mathematics as needed, and it is generally well-illustrated, which is generally not a feature of older engineering textbooks. There are problems at the end of each chapter. Unfortunately, though, answers are not included. It is definitely geared for the upper-level undergraduate engineering student that has already finished physics, calculus, statics, and dynamics. Highly recommended.
4 of 4 people found the following review helpful.
Classic Book, in depth analysis, relevant and useful
By RentNetguru
Dover books are typically designed to last and this is no exception. Much of the work behind Theory of Flight came before World War II, materials and technology substantially advanced since then. However, the detail and depth of understanding offered by this book is definitely worthy of consideration. One may read it without plunging into the calculus but to really understand it, if you aren't fresh (in a year's calculus) bring a college calc text for company. That said, the scope of this book is relevant for modern subsonic airplane engineering and design. Upcoming drone or UAV model builders can gain insight for practical application from this book but should be aware of its limitations in the lower Reynold's number or slower speed and smaller aircraft specialization.
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