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Fundamentals of Aerodynamics

6th Edition

John D. Anderson Jr.

Publisher: McGraw-Hill Education

ISBN: 9781259129919

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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.

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

Given: Pressure p=1.9×104Ν/m2 Temperature T=203 Κ Gas constant R=287 J/(Kg. K) Calculation: The...Assume the following arbitrary shaped body. Consider an elemental area ds on the control surface,...Given Information: Flow type is irrotational. Calculation: Considering steady and inviscid flow: x...Given Information: The velocity of free stream = 50 ft/s The angle of attack = 4° The chord of...Using Biot savrat law; dV→ = Γ4πdl→×r→|r→|3 Now, Velocity induced at the center; V→= ∫ Γ 4π d l → ×...Formula used: The flow can be proved to be irrotational if the cross gradient of velocity is zero....Given Information: Pressure of missile at stagnation point is, Po=7.8 atmTemperature of missile at...Given: The temperature of air is T=230 K . Formula used: The expression for speed of sound is given...Given: The Mach number of slender missile is M=1.5 . The horizontal distance is H=559 ft . Formula...

Given: The Reservoir pressure is p0=5 atm . The Reservoir temperature is T0=520 °R . The ratio of...Given: The freestream velocity of the compressible flow is V∞=700 ft/s . The pressure of the...Given: The angle of attack is α1=5° . The Mach number is M∞=2.6 . Formula used: The expression for...Given: The Cartesian coordinate system at (x1,y1)=(0,0.0684) . The Cartesian coordinate system at...Given: The angle of attack is α1=5° . The angle of attack is α2=15° . The angle of attack is α3=30°...Given: The distance between the plates is h . The velocity of the top plate is ue . Formula used:...Given: The length of the wing is l=9.75 m . The chord of the wing is C=1.6 m . The cruising speed of...

Corresponding editions of this textbook are also available below:

Fundamentals of Aerodynamics

5 Edition

ISBN: 9780073398105

Fundamentals of Aerodynamics

5 Edition

ISBN: 9780077418083

FUNDAMENTALS OF AERODYNAMICS (V.1+2)

12 Edition

ISBN: 9781121504981

Package: Fundamentals Of Aerodynamics With 1 Semester Connect Access Card

6 Edition

ISBN: 9781259934063

ENG ME 421 AERODYNAMICS >CUSTOM<

17 Edition

ISBN: 9781308966960

EBK FUNDAMENTALS OF AERODYNAMICS

6 Edition

ISBN: 9781259681486

INTRO TO AERODYNAMICS>CUSTOM<

6 Edition

ISBN: 9781307195903

FUNDAMENTALS OF AERODYNAMICS-CONNECT

6 Edition

ISBN: 9781259683244

FUND. OF AERODYNAMICS-W/ACCESS

6 Edition

ISBN: 9781259978609

EBK FUNDAMENTALS OF AERODYNAMICS

6 Edition

ISBN: 8220103146609

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