Fundamentals of Aerodynamics - 6th Edition - by John D. Anderson Jr. - ISBN 9781259129919
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Fundamentals of Aerodynamics
6th Edition
John D. Anderson Jr.
Publisher: McGraw-Hill Education
ISBN: 9781259129919

Solutions for Fundamentals of Aerodynamics

Book Details

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.

Sample Solutions for this Textbook

We offer sample solutions for Fundamentals of Aerodynamics homework problems. See examples below:

Using Biot savrat law; dV→ = Γ4πdl→×r→|r→|3 Now, Velocity induced at the center; V→= ∫ Γ 4π d l → ×...Consider the Superrnarine Spitfire shown in Figure 5.19. The first version of the Spitfire was the...Prove that three-dimensional source flow is irrotational.Note: In the following problems, you will deal with both the International System of Units (SI) (N,...Note: In the following problems, you will deal with both the International System of Units (SI) (N,...Consider air at a temperature of 230 K. Calculate the speed of sound.Given: The upstream Mach number is M1=2.6 . The upstream static pressure is p1=1 atm . The upstream...A slender missile is flying at Mach 1.5 at low altitude. Assume the wave generated by the nose of...Consider an oblique shock wave with a wave angle of 30 in a Mach 4 flow. The upstream pressure and...Given: The Mach number is M1=4 . The pressure is p1=1 atm . Formula used: The expression for p0,1 is...The reservoir pressure and temperature for a convergent-divergent nozzle are 5 atm and 520R,...Consider a subsonic compressible flow in cartesian coordinates where the velocity potential is given...Using the results of linearized theory, calculate the lift and wave-drag coefficients for an...Given: The Cartesian coordinate system at (x1,y1)=(0,0.0684) . The Cartesian coordinate system at...Repeat Problem 9.13 using a. Newtonian theory b. Modified newtonian theory Compare these results...Given: The distance between the plates is h . The velocity of the top plate is ue . Formula used:...The wing on a Piper Cherokee general aviation aircraft is rectangular, with a span of 9.75 m and a...

More Editions of This Book

Corresponding editions of this textbook are also available below:

Fundamentals of Aerodynamics
5th Edition
ISBN: 9780073398105
6th Edition
ISBN: 9781265141387
6th Edition
ISBN: 9781266911842
Loose Leaf for Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259683992
6th Edition
ISBN: 9781259681486
Connect with LearnSmart for Anderson: Fundamentals of Aerodynamics, 6e
6th Edition
ISBN: 9781259683268

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