The following data was obtained from wind tunnel testing of a scale model: Air speed (m/s) Drag force (N) 0.00 1 0.44 2 2.04 4.97 4 9.36 5 15.30 To understand this data more universally and to understand the effects of viscosity, it would help to present this data nondimensionally as A) Froude number vs Mach number B) Weber number vs Euler number C) Drag coefficient vs Reynolds number D) Drag coefficient vs Froude number

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8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
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Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.8P
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The following data was obtained from wind tunnel testing of a scale model:
Air speed (m/s) Drag force (N)
0.00
1
0.44
2
2.04
4.97
4
9.36
5
15.30
To understand this data more universally and to understand the effects of viscosity, it would help to
present this data nondimensionally as
A) Froude number vs Mach number
B) Weber number vs Euler number
C) Drag coefficient vs Reynolds number
D) Drag coefficient vs Froude number
Transcribed Image Text:The following data was obtained from wind tunnel testing of a scale model: Air speed (m/s) Drag force (N) 0.00 1 0.44 2 2.04 4.97 4 9.36 5 15.30 To understand this data more universally and to understand the effects of viscosity, it would help to present this data nondimensionally as A) Froude number vs Mach number B) Weber number vs Euler number C) Drag coefficient vs Reynolds number D) Drag coefficient vs Froude number
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