2. Why the boundary condition of the airfoil surface (here ,we do an assumption, that th airfoil surface is assumed to a line, a camber line) is a streamline, and can be written in a mathematical equation: V + w'(s) = 0 ? 00,n

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 5.3P: Evaluate the Nusselt number for flow over a sphere for the following conditions: D=0.15m,k=0.2W/mK,...
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2. Why the boundary condition of the airfoil
surface (here ,we do an assumption, that the
airfoil surface is assumed to a line, a camber
line) is a streamline, and can be written in a
mathematical equation: V
+ w'(s) = 0 ?
00,n
Transcribed Image Text:2. Why the boundary condition of the airfoil surface (here ,we do an assumption, that the airfoil surface is assumed to a line, a camber line) is a streamline, and can be written in a mathematical equation: V + w'(s) = 0 ? 00,n
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