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Reynolds number using chord length in Flat Plate for Viscous Flow Case Formulas
Reynolds number using chord length, where the length is usually the chord length of an airfoil or the chord length of a wing. The chord length of a wing may vary from root to tip. And is denoted by Re
c
.
Formulas to find Reynolds number using chord length in Flat Plate for Viscous Flow Case
f
x
Reynolds Number for Chord Length
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f
x
Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient
Go
Flat Plate for Viscous Flow Case formulas that make use of Reynolds number using chord length
f
x
Static Density of Plate using Chord Length for Flat Plate Case
Go
f
x
Static Velocity of Plate using Chord Length for Flat Plate Case
Go
f
x
Chord Length for Flat Plate Case
Go
f
x
Static Viscosity of Plate using Chord Length for Flat Plate Case
Go
f
x
Overall Skin-Friction Drag Coefficient
Go
f
x
Overall Skin-Friction Drag Coefficient for Incompressible Flow
Go
List of variables in Flat Plate for Viscous Flow Case formulas
f
x
Static density
Go
f
x
Static Velocity
Go
f
x
Chord Length
Go
f
x
Static Viscosity
Go
f
x
Overall Skin-friction Drag Coefficient
Go
FAQ
What is the Reynolds number using chord length?
Reynolds number using chord length, where the length is usually the chord length of an airfoil or the chord length of a wing. The chord length of a wing may vary from root to tip.
Can the Reynolds number using chord length be negative?
{YesorNo}, the Reynolds number using chord length, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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