ENG ME 421 AERODYNAMICS >CUSTOM<17th EditionAnderson Publisher: MCG/CREATEISBN: 9781308966960
ENG ME 421 AERODYNAMICS >CUSTOM<
Solutions for ENG ME 421 AERODYNAMICS >CUSTOM<
Problem 1.1P:
For most gases at standard or near standard conditions, the relationship among pressure, density,...Problem 1.2P:
Starting with Equations (1.7),(1.8), and (1.11), derive in detail Equations (1.15),(1.16), and...Problem 1.3P:
Consider an infinitely thin flat plate of chord c at an angle of attack in a supersonic flow. The...Problem 1.4P:
Consider an infinitely thin flat plate with a 1 m chord at an angle of attack of 10 in a supersonic...Problem 1.5P:
Consider an airfoil at 12 angle of attack. The normal and axial force coefficients are 1.2 and 0.03,...Problem 1.6P:
Consider an NACA 2412 airfoil (the meaning of the number designations for standard NACA airfoil...Problem 1.7P:
The drag on the hull of a ship depends in part on the height of the water waves produced by the...Problem 1.8P:
The shock waves on a vehicle in supersonic flight cause a component of drag called supersonic wave...Problem 1.9P:
Consider two different flows over geometrically similar airfoil shapes, one airfoil being twice the...Problem 1.10P:
Consider a Lear jet flying at a velocity of 250 m/s at an altitude of 10 km. where the density and...Problem 1.11P:
A U-tube mercury manometer is used to measure the pressure at a point on the wing of a wind-tunnel...Problem 1.12P:
The German Zeppeins of World War I were dirigibles with the following typical characteristics:...Problem 1.13P:
Consider a circular cylinder in a hypersonic flow, with its axis perpendicular to the flow. Let be...Problem 1.14P:
Derive Archimedes principle using a body of general shape.Problem 1.15P:
Consider a light, single-engine, propeller-driven airplane similar to a Cessna Skylanc. The airplane...Problem 1.16P:
Consider a flat plate at zero angle of attack in a hypersonic flow at Mach10 at standard sea level...Problem 1.17P:
Consider the Space Shuttle during its atmospheric entry at the end of a mission in space. At the...Problem 1.18P:
The purpose of this problem is to give you a feel for the magnitude of Reynolds number appropriate...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
Sample Solutions for this Textbook
We offer sample solutions for ENG ME 421 AERODYNAMICS >CUSTOM< 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
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ISBN: 9781265141387
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Loose Leaf for Fundamentals of Aerodynamics
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ISBN: 9781259683992
EBK FUNDAMENTALS OF AERODYNAMICS
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ISBN: 9781259681486
INTRO TO AERODYNAMICS>CUSTOM<
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FUNDAMENTALS OF AERODYNAMICS-CONNECT
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ISBN: 8220103146609
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