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Modern Compressible Flow: With Historical Perspective
 
 
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Modern Compressible Flow: With Historical Perspective [Hardcover]

John Anderson (Author)
4.5 out of 5 stars  See all reviews (10 customer reviews)

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Book Description

0072424435 978-0072424430 July 19, 2002 3
Anderson's book provides the most accessible approach to compressible flow for Mechanical and Aerospace Engineering students and professionals. In keeping with previous versions, the 3rd edition uses numerous historical vignettes that show the evolution of the field. New pedagogical features--"Roadmaps" showing the development of a given topic, and "Design Boxes" giving examples of design decisions--will make the 3rd edition even more practical and user-friendly than before. The 3rd edition strikes a careful balance between classical methods of determining compressible flow, and modern numerical and computer techniques (such as CFD) now used widely in industry & research. A new Book Website will contain all problem solutions for instructors.

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Editorial Reviews

About the Author

John D. Anderson, Jr. is the Curator of Aerodynamics at the National Air & Space Museum Smithsonian Institute and Professor Emeritus at the University of Maryland.

Product Details

  • Hardcover: 776 pages
  • Publisher: McGraw-Hill Science/Engineering/Math; 3 edition (July 19, 2002)
  • Language: English
  • ISBN-10: 0072424435
  • ISBN-13: 978-0072424430
  • Product Dimensions: 9.5 x 7.7 x 1.3 inches
  • Shipping Weight: 2.9 pounds (View shipping rates and policies)
  • Average Customer Review: 4.5 out of 5 stars  See all reviews (10 customer reviews)
  • Amazon Best Sellers Rank: #100,146 in Books (See Top 100 in Books)

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Customer Reviews

10 Reviews
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Average Customer Review
4.5 out of 5 stars (10 customer reviews)
 
 
 
 
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Most Helpful Customer Reviews

18 of 19 people found the following review helpful:
5.0 out of 5 stars The best engineering book I have ever read, April 20, 2001
By A Customer
This book was an indispensible study tool for my PhD qualifying exam in high temp gas dynamics. Before reading this book I had never had a formal compressible flow class and I think that it covers the fundamental concepts of frozen compressible flow very well. If you don't have an excellent understanding of normal and oblique shocks, expansion fans, nozzle flow, blunt body flow and shock tubes after reading this book, you haven't been paying attention!
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13 of 14 people found the following review helpful:
3.0 out of 5 stars a little disappointing, January 19, 2000
Well written classic supersonic theory, but "flavor" of numerical methods is given only : I think a college textbook of that price should give more than just flavor. Classic supersonic theory is not complete and needs to be integrated with other prior classic books (i.e. Ferri, Aerodynamics of supersonic flows). Overally, a little disappointing about the quantity of information given.
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9 of 10 people found the following review helpful:
4.0 out of 5 stars Heavy in math, but illustrations and commentary helps., September 14, 1999
By A Customer
As it must be, this book is heavy in math, yet does not treat the subject just from a mathmatics point of view. It is filled with illustrations, photographs and commentary to help explain the subject matter. The only thing that seems to be missing is a math symbols list! It's a good text, well written and worth the money.
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Inside This Book (learn more)
First Sentence:
Modern life is fast-paced. Read the first page
Key Phrases - Statistically Improbable Phrases (SIPs): (learn more)
nonequilibrium nozzle flows, flowfield variables, supersonic blunt body problem, induced mass motion, vortical singularity, compressible flow applications, equilibrium chemically reacting mixture, oblique shock diffuser, vortical singularities, incident expansion wave, equilibrium chemically reacting gas, calorically perfect gas, rearward differences, entropy streamline, subsonic inflow boundary, velocity potential equation, oblique shock properties, oblique shock theory, unsteady wave motion, hypersonic similarity, flowfield values, blunt body flowfield, nonequilibrium expansion, normal shock properties, locally supersonic flow
Key Phrases - Capitalized Phrases (CAPs): (learn more)
United States, Solution From Table, World War, Theodore von Karman, Adolf Busemann, Isaac Newton, John Stack, Substitute Eqs, Air Force, Ludwig Prandtl, Jet Propulsion Engine Thrust, Leonhard Euler, Technische Hochschule, Cal Tech, Daniel Bernoulli, English Engineering System, Langley Aeronautical Laboratory, New York, Proceedings of the Royal Society, Solution From Example, Some Theoretical Aspects of Transonic Flows, The Basics, After Anderson, Examine Eqs, General Conservation Equations Revisited
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