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Fundamentals of Aerodynamics 6/e

作者：John Anderson
原價：NT$ 1,150

ISBN：9781259251344
版次：6
年份：2017
出版商：McGraw-Hill
頁數/規格：1130頁/平裝雙色

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Description
Fundamentals of Aerodynamics is meant to be read. The writing style is intentionally conversational in order to make the book easier to read. The book is designed to talk to the reader; in part to be a self-teaching instrument. Learning objectives have been added to each chapter to reflect what is believed to be the most important items to learn from that particular chapter. This edition emphasizes the rich theoretical and physical background of aerodynamics, and marbles in many historical notes to provide a background as to where the aerodynamic technology comes from. Also, new with this edition, are "Integrated Work Challenges" that pertain to the chapter as a whole, and give the reader the opportunity to integrate the material in that chapter, in order to solve a "bigger picture".

McGraw-Hill Education's Connect, is also available as an optional, add on item. Connect is the only integrated learning system that empowers students by continuously adapting to deliver precisely what they need, when they need it, how they need it, so that class time is more effective. Connect allows the professor to assign homework, quizzes, and tests easily and automatically grades and records the scores of the student's work. Problems are randomized to prevent sharing of answers an may also have a "multi-step solution" which helps move the students' learning along if they experience difficulty.

Features

Connect: A highly reliable, easy-to-use homework and learning management solution that embeds learning science and award-winning adaptive tools to improve student results.

A conversational, self-teaching narrative guides students through learning objectives in each chapter, preparing them to tackle “Integrated Work Challenges” that provide practice in solving big picture problems.

This edition emphasizes both the theoretical and the physical background of aerodynamics.

Table of Contents
Part One - Fundamental Principles
1) Aerodynamics: Some Introductory Thoughts
2) Aerodynamics: Some Fundamental Principles and Equations

Part Two - Inviscid, Incompressible Flow
3) Fundamentals of Inviscid, Incompressible Flow
4) Incompressible Flow over Airfoils
5) Incompressible Flow over Finite Wings
6) Three-Dimensional Incompressible Flow

Part Three - Inviscid, Compressible Flow
7) Compressible Flow: Some Preliminary Aspects
8) Normal Shock Waves and Related Topics
9) Oblique Shock and Expansion Waves
10) Compressible Flow Through Nozzles, Diffusers, and Wind Tunnels
11) Subsonic Compressible Flow over Airfoils: Linear Theory
12) Linearized Supersonic Flow
13) Introduction to Numerical Techniques for Nonlinear Supersonic Flow
14) Elements of Hypersonic Flow

Part Four - Viscous Flow
15) Introduction to the Fundamental Principles and Equations of Viscous Flow
16) Some Special Cases; Couette and Poiseuille Flows
17) Introduction to Boundary Layers
18) Laminar Boundary Layers
19) Turbulent Boundary Layers
20) Navier-Stokes Solutions: Some Examples

Appendix A - Isentropic FlowProperties
Appendix B - Normal Shock Properties
Appendix C - Prandtl-Meyer Function and Mach Angle
Appendix D - Standard Atmosphere, SI Units
Appendix E - Standard Atmosphere, English Engineering Units

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