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.
Les mer
Part One - Fundamental Principles1) Aerodynamics: Some Introductory Thoughts2) Aerodynamics: Some Fundamental Principles and EquationsPart Two - Inviscid, Incompressible Flow3) Fundamentals of Inviscid, Incompressible Flow4) Incompressible Flow over Airfoils5) Incompressible Flow over Finite Wings6) Three-Dimensional Incompressible FlowPart Three - Inviscid, Compressible Flow7) Compressible Flow: Some Preliminary Aspects8) Normal Shock Waves and Related Topics9) Oblique Shock and Expansion Waves10) Compressible Flow Through Nozzles, Diffusers, and Wind Tunnels11) Subsonic Compressible Flow over Airfoils: Linear Theory12) Linearized Supersonic Flow13) Introduction to Numerical Techniques for Nonlinear Supersonic Flow14) Elements of Hypersonic FlowPart Four - Viscous Flow15) Introduction to the Fundamental Principles and Equations of Viscous Flow16) Some Special Cases; Couette and Poiseuille Flows17) Introduction to Boundary Layers18) Laminar Boundary Layers19) Turbulent Boundary Layers20) Navier-Stokes Solutions: Some ExamplesAppendix A - Isentropic FlowPropertiesAppendix B - Normal Shock PropertiesAppendix C - Prandtl-Meyer Function and Mach AngleAppendix D - Standard Atmosphere, SI UnitsAppendix E - Standard Atmosphere, English Engineering Units
Les mer
Produktdetaljer
ISBN
9781259251344
Publisert
2016-04-16
Utgave
6. utgave
Utgiver
Vendor
McGraw-Hill Education
Vekt
1445 gr
Høyde
231 mm
Bredde
188 mm
Dybde
38 mm
Aldersnivå
P, 06
Språk
Product language
Engelsk
Format
Product format
Heftet
Antall sider
2304
Forfatter