100 Data scatter Percentage of pressure drag (a) 0.2 0.4 0.6 0.8 1.0 Circular cylinder 0.3 Cp based on frontal area (tb) 0.2 Cp based on planform area (cb) Cp 0.1 - Width b Flat plate (b) 0.2 0.4 0.6 0.8 1.0 Thickness ratio Friction drag percent
100 Data scatter Percentage of pressure drag (a) 0.2 0.4 0.6 0.8 1.0 Circular cylinder 0.3 Cp based on frontal area (tb) 0.2 Cp based on planform area (cb) Cp 0.1 - Width b Flat plate (b) 0.2 0.4 0.6 0.8 1.0 Thickness ratio Friction drag percent
Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
Publisher:Kreith, Frank; Manglik, Raj M.
Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.49P
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The drag of an airfoil (Fig.) increases considerably if
you turn the sharp edge around 180° to face the stream. Can
you explain this?
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