A Method of Correcting the Wind Resistance Characteristics of Lubricating Oil Radiator
A technology of air resistance characteristics and radiators, which is applied in the direction of instruments, special data processing applications, geometric CAD, etc., and can solve the problem of the deviation of the ground wind resistance characteristic curve of the oil radiator, the performance of the oil heat dissipation system that cannot meet the design requirements, and the performance that cannot be met Analyze requirements and other issues to achieve the effect of eliminating errors and avoiding substandard performance
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Embodiment 1
[0025] It is necessary to correct the wind resistance characteristic curve of a certain type of air-cooled oil radiator on board, the specific steps are as follows:
[0026] 1. Obtain the basic data of the air resistance characteristics of the oil radiator:
[0027] Through the ground ventilation test, the wind resistance characteristics of this type of lubricating oil radiator under standard atmospheric conditions at sea level are obtained, as shown in the formula [1]:
[0028] Δp=0.32·Q m 2 +0.115 Q m ……[1]
[0029] Among them, the ventilation rate Q m The unit of is kg / s, and the unit of wind resistance Δp is kPa.
[0030] 2. Calculate the air resistance Δp of the oil radiator after correction:
[0031] When the flight altitude of the aircraft is 6000m, look up the table to obtain the air density ρ at this altitude ∞ =0.6601kg / m 3 , the coefficient of aerodynamic viscosity μ ∞ =1.595×10 -5 Pa·s, air density ρ at sea level 0 =1.225kg / m 3 , the coefficient of aero...
Embodiment 2
[0038] It is necessary to correct the wind resistance characteristic curve of a certain type of air-cooled oil radiator on board, the specific steps are as follows:
[0039] 1. Obtain the basic data of the air resistance characteristics of the oil radiator:
[0040] Through the ground ventilation test, the wind resistance characteristics of this type of lubricating oil radiator under standard atmospheric conditions at sea level are obtained, as shown in formula (1):
[0041] Δp=0.5525·Q m 1.6 ……[1]
[0042] Among them, the ventilation rate Q m The unit of is kg / s, and the unit of wind resistance Δp is kPa.
[0043] 2. Calculate the air resistance Δp of the oil radiator after correction:
[0044] When the flight altitude of the aircraft is 4500m, look up the table to obtain the air density ρ at this altitude ∞ =0.7770kg / m 3 , the coefficient of aerodynamic viscosity μ ∞ =1.645×10 -5 Pa·s, air density ρ at sea level 0 =1.225kg / m 3 , the coefficient of aerodynamic visc...
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