Fundamentals of Aerodynamics https://www.mheducation.com/cover-images/Jpeg_400-high/1259129918.jpeg 6 9781259129919 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'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.
Fundamentals of Aerodynamics

Fundamentals of Aerodynamics

6th Edition
By John Anderson
ISBN10: 1259129918
ISBN13: 9781259129919
Copyright: 2017
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09781259129919

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Program Details

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