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Mechanics of Flight, by Warren F Phillips
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Mechanics of Flight
- Sales Rank: #1243097 in Books
- Published on: 2012
- Original language: English
- Dimensions: .0" h x .0" w x .0" l, 3.55 pounds
- Binding: Paperback
- 1152 pages
Most helpful customer reviews
26 of 26 people found the following review helpful.
If you study or design aircraft, you must have this book
By A Customer
"Mechanics of Flight" will become a classic in the aerodynamicist's library alongside Abbott and Von Doenhoff's "Theory of Wing Sections". Here's why:
* Coverage of topics in aircraft design is exhaustive. From balancing lift and weight for steady flight, on through off axis forces and moments from running propellers, to 6-dof formulas for aircraft dynamic modes, to how propeller location affects aircraft stability, and on and on. Great for both the beginner and the authority in aircraft.
* Often a completely thorough analysis including the minutest effects is presented along with a linearized or simplified method. The simplified analysis is so useful for rapid conceptual design and study of fundamentals, while the detailed analysis gives a complete grasp of the physics and phenomena involved. Plus, in simplifying a complex derivation, the reader is shown which parameters may be safely neglected and which require careful scrutiny, and what is engineering if not intelligently ignoring smaller effects to come up with a reasonable solution to a problem?
* The figures! Well thought out and consistent, the figures clearly illustrate the material.
* Actual aircraft data is used in the example and homework problems. I have a feel for the performance of several classes of aircraft simply from using this book.
* Phillips derives everything, and I mean everything using the fundamental laws of physics as the starting point. A student would be very well served to go through these derivations themselves. Phillips basically shows the student how to learn and how to think mathematically. No shortcuts here. I wish I had learned these things very early on in my own schooling.
* Phillips has included experimental data along with rigorous analytical derivation and computer numerical analysis. I believe that all three are necessary for a true understanding of fluid dynamics.
The bottom line: Buy and use this book! While it is true that the material is focused on subsonic flight, I work for a large airframer of supersonic aircraft and I find the principles and fundamentals to be extremely useful in my work. Whether you are a student or a professional, if you have an interest in aerodynamics this is THE book to use.
10 of 10 people found the following review helpful.
The Complete Resource for Engineers, Pilots & Homebuilders
By B. Santana
"Mechanics of Flight" is an excellent textbook for students of aeronautics as well as an invaluable reference for engineers practicing in aerospace, experimental homebuilders, and pilots having a flare for science. The subject matter is well-organized, thorough in coverage, comprehensively indexed, and has an impressive bibliography. There are numerous worked examples, excellent graphics to illustrate concepts, and many aeronautical/aerodynamic relationships are plotted to demonstrate parametric relationships. Numerical solution techniques are discussed throughout the book and many problems are tailored for a programmed solution on a digital computer. Although this is a textbook, and the concepts are demonstrated using rigorous mathematical derivations, considerable insight into the mechanics of flight can be gained by simply reading the text, studying the figures and absorbing the numerous tips and rules of thumb. The reader is taken from overviews of aerodynamics and propulsion in the first two chapters through aircraft performance, aircraft controls and maneuverability, static stability and control, aircraft dynamics, handling qualities, and closing with aircraft flight simulation.
Prandtl's classical lifting-line method is the basis for much of the aerodynamic theory used in the book. The author uses the method to explore lift and drag for various wing planforms. He further develops the effects of geometric and/or aerodynamic twist and how induced drag is affected. A significant result shown is that there is an optimum washout distribution for any wing planform which will minimize induced drag. The author has also generalized lifting-line theory to allow study of the effects of wing sweep, dihedral and interaction between lifting surfaces. The method is about 4 orders of magnitude faster than panel methods and 6 orders of magnitude faster than CFD solutions. The numerical lifting-line method with parasitic drag included provides a computationally efficient method for preliminary aircraft design.
The author has presented a particularly thorough discussion of propeller theory in Chapter 2. This section may be of particular interest to pilots. Fixed-pitch and constant-speed propellers histories are included and their mechanical attributes and efficiency compared. The reader gains considerable insight into how a propeller does its job and how one might select a certain propeller for a particular aircraft and mission. Both Goldstein's vortex theory and the more common propeller momentum theory are developed by the author. He has also shown how momentum theory can be improved by incorporating slipstream rotation. The chapter on aircraft performance also provides practical insight on fuel consumption, endurance, and range. Numerous worked examples show how these parameters change with gross weight and wind, illustrating the mathematical equations with plots to simplify the information. The section on takeoff and landing performance may be of special interest to homebuilders and pilots.
The chapters on static stability and trim will also be of interest to the homebuilder. Simplified pitch stability analysis is presented for standard wing-tail and wing-canard combinations, which are useful for preliminary aircraft design as well as an estimate for downwash angle on an aft tail. Many factors affecting pitch stability and their effects are discussed in detail, including the contribution of a running propeller, and its location, on the static stability of an airplane. Lateral stability is treated with equal aplomb and some rules of thumb for aircraft design are provided. Longitudinal-lateral coupling, such as the yawing moment produced by a rotating propeller, is described and the designer alerted to the fact that static stability cannot always be separated into longitudinal and lateral motion.
Chapter 7 provides a more general formulation of the rigid-body equations of motion than presented in the preceding chapters. This chapter will thrill the mathematics enthusiast! It starts with a review of mathematical notation and coordinate systems and proceeds to develop Newton's second law for rigid-body dynamics. Ultimately, the nondimensional linearized equations of motion are derived for a symmetric configuration after applying the small disturbance approximation. The last section of this chapter discusses how inertial and gyroscopic coupling come into play if symmetry is relaxed.
Linearized longitudinal and lateral dynamics are examined in Chapters 8 and 9 and the eigenvalues obtained from the solution of the eigenvalue problem are related to the phugoid, Dutch roll, etc. Longitudinal-lateral coupling in the equations of motion is addressed by solving the full 12x12 eigen-problem associated with linearized aircraft dynamics. It is shown that a flight condition as simple as turning flight introduces this coupling, which cannot be fully analyzed using the uncoupled equations.
I personally found the comprehensive presentation of the quaternion formulation for 6-DOF flight simulation, which is presented in Chapter 11, to be unique, interesting, and understandable. This information is not available in any other single source to the best of my knowledge.
It is not possible in this brief space to do justice to the comprehensive coverage of flight mechanics provided by this textbook. The book is rich in aircraft history, modern approaches to classical solution methods and new ways to look at well-founded theories. The only possible shortcoming that I could find was the need to make my way through the challenging mathematics that supports the concepts (not necessarily a bad thing for a textbook). It will be a resource used for many years by students, practicing engineers, experimental homebuilders, pilots, and maybe even model airplane enthusiasts. This book may be destined to become a classic in the field!
7 of 7 people found the following review helpful.
An absolute masterpiece!
By N. Alley
Warren Phillips has broken the mold with this book. I am currently a Doctoral candidate in aerospace engineering and I found his use of examples and ability to clearly explain complex topics to be unparalleled in any other text. Myths and misunderstandings about flight mechanics that have propagated down through decades of other texts are disproved or clarified. Dr. Phillips clearly understands and has thoroughly researched each topic that he presents, as the reader is never left in the dark by the ambiguous "hand-waiving" so common in other texts.
For professionals, the exhaustive index and methodical explanations make Mechanics of Flight the ideal reference.
For students in mechanical, aeronautical, or aerospace engineering, there has never been available a more student friendly text for learning flight mechanics and flight simulation.
For engineering professors, using this book will make teaching any senior or graduate level flight mechanics or flight simulation class easier for you and more enlightening for your students. Additionally, an amazing 592 page solutions manual is available from the publisher!
This book is a must buy and I predict that Mechanics of Flight by Warren F. Phillips will soon be recognized by the engineering community as the "bible" of sub-sonic flight mechanics.
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