SDP3x: Add model for pitot pressure drop

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Lorenz Meier 2017-07-26 09:26:15 +02:00
parent ae1f8381ce
commit 98bd6e43e8
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"""
Copyright (c) 2017, Sensirion AG
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"""
import numpy as np
import matplotlib.pyplot as plt
## differential pressure, sensor values in Pascal
dp_SDP33=np.linspace(0,800,100)
## total length tube in mm = length dynamic port+ length static port; compensation only valid for inner diameter of 1.5mm
l_tube=400
## densitiy air in kg/m3
rho_air=1.29
## flow through sensor
flow_SDP33=(300.805 - 300.878/(0.00344205*dp_SDP33**0.68698 + 1))*1.29/rho_air
## additional dp through pitot tube
dp_Pitot=28557670. - 28557670./(1 + (flow_SDP33/5027611)**1.227924)
## pressure drop through tube
dp_Tube=flow_SDP33*0.000746124*l_tube*rho_air
## speed at pitot-tube tip due to flow through sensor
dv=0.0331582*flow_SDP33
## sum of all pressure drops
dp_tot=dp_SDP33+dp_Tube+dp_Pitot
## computed airspeed without correction for inflow-speed at tip of pitot-tube
airspeed_uncorrected=np.sqrt(2*dp_tot/rho_air)
## corrected airspeed
airspeed_corrected=airspeed_uncorrected+dv
## just to compare to value without compensation
airspeed_raw=np.sqrt(2*dp_SDP33/rho_air)
plt.figure()
plt.plot(dp_SDP33,airspeed_corrected/airspeed_raw)
plt.xlabel('differential pressure raw value [Pa]')
plt.ylabel('correction factor [-]')
plt.show()
plt.figure()
plt.plot(airspeed_corrected,(airspeed_corrected-airspeed_raw)/airspeed_corrected)
plt.xlabel('airspeed [m/s]')
plt.ylabel('relative error [-]')
plt.show()