- #1
Thusithatck
- 13
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Can someone explain to me how XFoil calculates the Reynolds Number for computational analysis. I have the XFoil manual which explains the method used in calculating the Reynolds Number. But what I don't understand is that it says that the "Reynolds Number is defined with the freestream velocity and viscosity, and an implied unit chord.
My experimental data are,
Re,chord = 380,000
V = 16.67 m/s
T = 293 K
P = 101325 Pa
Viscosity = 1.813 e-5 kg/ms
Density = 1.205 kg/m3
above values are extracted from an experiment, where I'm intending to use XFoil for the validation of experimental data. According to the Reynolds Number equation mentioned below where,
Re = (V x density x chord) / viscosity
if the implied chord is taken as a unit, then the Reynolds number I should enter in XFoil should be 1107872 (not 380,000), approximately. Having said that, when it say freestream velocity and viscosity, does it mean I should use the velocity as 16.67 m/s (which is the correct speed of the wind tunnel during the experiment) and the sea level viscosity which is 1.78 e-5 (not 1.813 e-5, which is the correct density at the wind tunnel during the experiment).
Since the force coefficients (CL, CD, CM) are calculated (in XFoil) by normalizing the forces with ONLY the freestream dynamic pressure, which is given in below equation,
q = 0.5 x density x V2
CL = L / q
CD = D / q
Cm = M / q
where the only input parameter options available in XFoil are Reynolds Number and the Mach Number. Hence I believe that velocity in the dynamic pressure equation above is calculated from the Reynold number equation and the other parameters such as viscosity and density are taken as sea level conditions (not the experimental values). Therefore the Reynolds number has to be adjusted by using sea level values. Is this is correct ??
My experimental data are,
Re,chord = 380,000
V = 16.67 m/s
T = 293 K
P = 101325 Pa
Viscosity = 1.813 e-5 kg/ms
Density = 1.205 kg/m3
above values are extracted from an experiment, where I'm intending to use XFoil for the validation of experimental data. According to the Reynolds Number equation mentioned below where,
Re = (V x density x chord) / viscosity
if the implied chord is taken as a unit, then the Reynolds number I should enter in XFoil should be 1107872 (not 380,000), approximately. Having said that, when it say freestream velocity and viscosity, does it mean I should use the velocity as 16.67 m/s (which is the correct speed of the wind tunnel during the experiment) and the sea level viscosity which is 1.78 e-5 (not 1.813 e-5, which is the correct density at the wind tunnel during the experiment).
Since the force coefficients (CL, CD, CM) are calculated (in XFoil) by normalizing the forces with ONLY the freestream dynamic pressure, which is given in below equation,
q = 0.5 x density x V2
CL = L / q
CD = D / q
Cm = M / q
where the only input parameter options available in XFoil are Reynolds Number and the Mach Number. Hence I believe that velocity in the dynamic pressure equation above is calculated from the Reynold number equation and the other parameters such as viscosity and density are taken as sea level conditions (not the experimental values). Therefore the Reynolds number has to be adjusted by using sea level values. Is this is correct ??