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The 6th edition of 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. The 6th 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".
Now available with the sixth edition of Fundamentals of Aerodynamics, Connect. 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 your class time is more engaging and effective. Within Connect, SmartBook is available with the 6th edition as well. SmartBook is the first and only adaptive eBook for the Higher Education market. SmartBook facilitates the reading process by using practice questions to identify what content a student knows and doesn't know. As a student reads the text, the material continuously adapts to ensure that he or she is focused on the content most crucial to closing specific knowledge gaps.
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Contents
Part 1 Fundamental Principles
1- Aerodynamics: Some Introductory Thoughts
2- Aerodynamics: Some Fundamental Principles and Equations
Part 2 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 3 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 4 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 ShockProperties
Appendix C Prandtl-MeyerFunction and Mach Angle
Appendix D StandardAtmosphere, SI Units
Appendix E StandardAtmosphere, English Engineering Units
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Additional Information
ISBN (10-digit) 1259251349 ISBN 9781259251344 Authors N/A Edition 6 Series COLLEGE IE OVERRUNS Previous Edition's ISBN N/A Binding Paperback / softback Published 21 Mar 2016 Publication Status BACKLIST Stock Due 5 Apr 2019 Market N/A Division INTL Review Copy Available No Keywords N/A Format Print Availability Type None Blink Division N/A - Request a Review Copy