1997
DOI: 10.1007/s11666-997-0069-6
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Mathematical modeling of the gas and powder flow in HVOF systems

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Cited by 20 publications
(7 citation statements)
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“…28,29 From the exit of the nozzle to a position whose distance is not larger than the potential core length (L pc ), the gas velocity and temperature can be considered almost constant. 30 Further downstream, the gas velocity and temperature decay rapidly because of the entrainment of the surrounding air. This decay of the gas velocity and temperature can be described by the empirical formulas 30 and where x is the axial distance from the exit of the gun barrel (x > L pc ) and R and β are parameters obtained from experimental measurements.…”
Section: Modeling Of the Gas Thermal And Flowmentioning
confidence: 99%
“…28,29 From the exit of the nozzle to a position whose distance is not larger than the potential core length (L pc ), the gas velocity and temperature can be considered almost constant. 30 Further downstream, the gas velocity and temperature decay rapidly because of the entrainment of the surrounding air. This decay of the gas velocity and temperature can be described by the empirical formulas 30 and where x is the axial distance from the exit of the gun barrel (x > L pc ) and R and β are parameters obtained from experimental measurements.…”
Section: Modeling Of the Gas Thermal And Flowmentioning
confidence: 99%
“…It was assumed that adiabatic, isentropic and frictionless fluid flow conditions existed within this portion of the gun nozzle with a constant mean velocity and temperature. The mean axial gas temperature had the same functional form as the gas velocity (2) only with a larger exponential decay exponent (b T = 1.35), as proposed by Tawfik et al in 1997 [18]. It was also assumed that the predominant reaction product during the combustion of hydrogen and oxygen in the HVOF gun was water vapor, i.e.…”
Section: Hvof Gas Flow and Thermal Fieldsmentioning
confidence: 85%
“…Tawfik et al [18] proposed and experimentally verified empirical correlations for jet core length after the nozzle exit and the axial mean velocity (v (g) ) of an HVOF jet with a range of validity between Mach number 0.3 and 1.4. The jet core length is a function of the nozzle exit diameter (D NZL ) and local Mach number (Ma), as shown in Eq.…”
Section: Hvof Gas Flow and Thermal Fieldsmentioning
confidence: 99%
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“…For the external flow and thermal fields, empirical formulae are used for the gas velocity and temperature decay, [18] which are experimentally derived as functions of the distance from the exit of the HVOF gun.…”
Section: Modeling Of Gas Flow and Thermal Fieldsmentioning
confidence: 99%