EBK FUNDAMENTALS OF AERODYNAMICS6th EditionAnderson Publisher: MCGRAW HILL BOOK COMPANYISBN: 9781259681486
EBK FUNDAMENTALS OF AERODYNAMICS
Solutions for EBK FUNDAMENTALS OF AERODYNAMICS
Problem 2.1P:
Consider a body of arbitrary shape. If the pressure distribution over the surface of the body is...Problem 2.2P:
Consider an airfoil in a wind tunnel (i.e., a wing that spans the entire test section). Prove that...Problem 2.3P:
Consider a velocity field where the x and y components of velocity are given by u=cx/(x2+y2) and...Problem 2.4P:
Consider a velocity field where the x and y components of velocity are given by u=cy/(x2+y2) and...Problem 2.5P:
Consider a velocity field where the radial and tangential components of velocity arc Vr=0 and V=cr,...Problem 2.6P:
Consider a velocity field where the x and y components of velocity are given by u=cx and v=cy, where...Problem 2.7P:
The velocity field given in Problem 2.3 is called source flow, which will be discussed in Chapter 3....Problem 2.8P:
The velocity field given in Problem 2.4 is called vortex flow, which will be discussed in Chapter 3....Problem 2.10P:
Consider a flow field in polar coordinates, where the stream function is given as =(r,). Starting...Problem 2.11P:
Assuming the velocity field given in Problem 2.6 pertains to an incompressible flow, calculate the...Problem 2.12P:
Consider a length of pipe bent into a U-shape. The inside diameter of the pipe is 0.5 m. Air enters...Browse All Chapters of This Textbook
Chapter 1 - Aerodynamics: Some Introductory ThoughtsChapter 2 - Aerodynamics: Some Fundamental Principles And EquationsChapter 3 - Fundamentals Of Inviscid, Incompressible FlowChapter 4 - Incompressible Flow Over AirfoilsChapter 5 - Incompressible Flow Over Finite WingsChapter 6 - Three-dimensional Incompressible FlowChapter 7 - Compressible Flow: Some Preliminary AspectsChapter 8 - Normal Shock Waves And Related TopicsChapter 9 - Oblique Shock And Expansion WavesChapter 10 - Compressible Flow Through Nozzles, Diffusers, And Wind Tunnels
Chapter 11 - Subsonic Compressible Flow Over Airfoils: Linear TheoryChapter 12 - Linearized Supersonic FlowChapter 13 - Introduction To Numerical Techniques For Nonlinear SupersonicChapter 14 - Elements Of Hypersonic FlowChapter 15 - Introduction To The Fundamental Principles And Equations Of VisChapter 19 - Turbulent Boundary Layers
Book Details
With this new edition the successful pedagogical features such as chapter roadmaps preview boxes design boxes and summary sections are continued in order to motivate the reader to be excited about the subject and to want to learn the material. This book i
Sample Solutions for this Textbook
We offer sample solutions for EBK FUNDAMENTALS OF AERODYNAMICS homework problems. See examples below:
Chapter 1, Problem 1.1PChapter 1, Problem 1.2PChapter 1, Problem 1.4PChapter 2, Problem 2.1PChapter 2, Problem 2.11PChapter 3, Problem 3.1PChapter 3, Problem 3.23PChapter 4, Problem 4.1PChapter 4, Problem 4.9P
Chapter 5, Problem 5.1PChapter 5, Problem 5.9PChapter 6, Problem 6.1PChapter 7, Problem 7.1PChapter 7, Problem 7.2PChapter 8, Problem 8.1PChapter 8, Problem 8.7PChapter 9, Problem 9.1PChapter 9, Problem 9.2PChapter 9, Problem 9.8PChapter 10, Problem 10.1PChapter 11, Problem 11.1PChapter 12, Problem 12.1PChapter 13, Problem 13.1PChapter 14, Problem 14.1PChapter 15, Problem 15.1PChapter 19, Problem 19.1P
More Editions of This Book
Corresponding editions of this textbook are also available below:
Fundamentals of Aerodynamics
5th Edition
ISBN: 9780073398105
Fundamentals of Aerodynamics
5th Edition
ISBN: 9780077418083
FUNDAMENTALS OF AERODYNAMICS (V.1+2)
12th Edition
ISBN: 9781121504981
Package: Fundamentals Of Aerodynamics With 1 Semester Connect Access Card
6th Edition
ISBN: 9781259934063
Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
FUND OF AERODYNAMICS(LLF) +CONNECT (1YR)
6th Edition
ISBN: 9781265141387
FUND OF AERODYNAMICS--CONNECT (360 DAYS)
6th Edition
ISBN: 9781266911842
ENG ME 421 AERODYNAMICS >CUSTOM<
17th Edition
ISBN: 9781308966960
Loose Leaf for Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259683992
INTRO TO AERODYNAMICS>CUSTOM<
6th Edition
ISBN: 9781307195903
FUNDAMENTALS OF AERODYNAMICS-CONNECT
6th Edition
ISBN: 9781259683244
FUND. OF AERODYNAMICS-W/ACCESS
6th Edition
ISBN: 9781259978609
EBK FUNDAMENTALS OF AERODYNAMICS
6th Edition
ISBN: 8220103146609
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