EBK FUNDAMENTALS OF AERODYNAMICS6th EditionAnderson Publisher: MCGRAW HILL BOOK COMPANYISBN: 9781259681486
EBK FUNDAMENTALS OF AERODYNAMICS
Solutions for EBK FUNDAMENTALS OF AERODYNAMICS
Problem 3.1P:
For an irrotational flow. show that Bernoullis equation holds between any points in the flow, not...Problem 3.2P:
Consider a venturi with a throat-to-inlet area ratio of 0.8, mounted on the side of an airplane...Problem 3.3P:
Consider a venturi with a small hole drilled in the side of the throat. This hole is connected via a...Problem 3.4P:
Consider a low-speed open-circuit subsonic wind tunnel with an inlet-to-throat area ratio of 12. The...Problem 3.5P:
Assume that a Pitot tube is inserted into the test-section flow of the wind tunnel in Problem 3.4....Problem 3.6P:
A Pilot tube on an airplane flying at standard sea level reads 1.07105N/m2. What is the velocity of...Problem 3.7P:
At a given point on the surface of the wing of the airplane in Problem 3.6, the flow velocity is 130...Problem 3.8P:
Consider a uniform flow with velocity V. Show that this flow is a physically possible incompressible...Problem 3.9P:
Show that a source flow is a physically possible incompressible flow everywhere except at the...Problem 3.10P:
Prove that the velocity potential and the stream function for a uniform flow, Equations (3.53)...Problem 3.11P:
Prove that the velocity potential and the stream function for a source flow, Equations (3.67)...Problem 3.12P:
Consider the flow over a semi-infinite body as discussed in Section 3.11. If V is the velocity of...Problem 3.13P:
Derive Equation (3.81). Hint: Make use of the symmetry of the flow field shown in Figure 3.18; thai...Problem 3.14P:
Derive the velocity potential for a doublet; that is, derive Equation (3.88). Hint: The easiest...Problem 3.15P:
Consider the nonlifting flow over a circular cylinder. Derive an expression for the pressure...Problem 3.16P:
Consider the nonlifting flow over a circular cylinder of a given radius, where V=20ft/s. If V is...Problem 3.17P:
Consider the lifting flow over a circular cylinder of a given radius and with a given circulation....Problem 3.18P:
The lift on a spinning circular cylinder in a freestream with a velocity of 30 m/s and at standard...Problem 3.19P:
A typical World War I biplane fighter (such as the French SPAD shown in Figure 3.50) has a number of...Problem 3.20P:
The Kutta-Joukowski theorem, Equation (3.140), was derived exactly for the case of the lifting...Problem 3.21P:
Consider the streamlines over a circular cylinder as sketched at the right of Figure 3.26. Single...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
Connect with LearnSmart for Anderson: Fundamentals of Aerodynamics, 6e
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