EBK FUNDAMENTALS OF AERODYNAMICS6th EditionAnderson Publisher: MCGRAW HILL BOOK COMPANYISBN: 9781259681486
EBK FUNDAMENTALS OF AERODYNAMICS
Solutions for EBK FUNDAMENTALS OF AERODYNAMICS
Problem 9.1P:
A slender missile is flying at Mach 1.5 at low altitude. Assume the wave generated by the nose of...Problem 9.2P:
Consider an oblique shock wave with a wave angle of 30 in a Mach 4 flow. The upstream pressure and...Problem 9.3P:
Equation (8.80) does not hold for an oblique shock wave, and hence the column in Appendix B labeled...Problem 9.4P:
Consider an oblique shock wave with a wave angle of 36.87. The upstream flow is given by M1=3 and...Problem 9.5P:
Consider the flow over a 22.2 half-angle wedge. If M1=2.5, p1=1atm, and T1=300K, calculate the wave...Problem 9.6P:
Consider a flat plate at an angle of attack a to a Mach 2.4 airflow at 1 atm pressure. What is the...Problem 9.7P:
A 30.2 half-angle wedge is inserted into a freestream with M=3.5 and P=0.5atm. A Pilot tube is...Problem 9.8P:
Consider a Mach 4 airflow at a pressure of 1 atm. We wish to slow this flow to subsonic speed...Problem 9.9P:
Consider an oblique shock generated at a compression corner with a deflection angle =18.2. A...Problem 9.10P:
Consider the supersonic flow over an expansion corner, such as given in Figure 9.25. The deflection...Problem 9.11P:
A supersonic flow at M1=1.58 and p1=1atm expands around a sharp corner. If the pressure downstream...Problem 9.12P:
A supersonic flow at M1=3,T1=285K, and p1=1atm is deflected upward through a compression corner with...Problem 9.13P:
Consider an infinitely thin flat plate at an angle of attack in a Mach 2.6 flow. Calculate the lift...Problem 9.14P:
Consider a diamond-wedge airfoil such as shown in Figure 9.36, with a half-angle =10. The airfoil is...Problem 9.15P:
Consider sonic flow. Calculate the maximum deflection angle through which this flow can be expanded...Problem 9.16P:
Consider a circular cylinder (oriented with its axis perpendicular to the flow) and a symmetric...Problem 9.17P:
Consider the supersonic flow over a flat plate at an angle of attack, as sketched in Figure 9.35. As...Problem 9.18P:
(The purpose of this problem is to calculate a two-dimensional expanding supersonic flow and compare...Problem 9.19P:
Repeat Problem 9.18, except with =30. Again, we will use these results to compare with a...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
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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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