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Effect of gas type on the thermal properties of small sonic nozzles

机译:气体型对小声灼喷嘴热特性的影响

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A previous study (Bignell and Choi, Flow Meas. & Instrum. 13 (2002) 17-22) of the effect of temperature on the coefficient used to characterise small sonic nozzles is reviewed. Adiabatic cooling of the gas stream in the throat causes the body of nozzles to be cooled but a heater and temperature control system allow the temperature of the nozzle to be held constant. Using a gas flow standard that can operate in continuous mode, measurements were made of nozzle coefficients at different temperatures using air, argon, nitrogen and carbon dioxide. The nozzle coefficient changes with the gas type and linearly with the temperature of the body of the nozzle. The first of these changes is explained by changes in the real gas correction factor for argon but not for carbon dioxide. The temperature changes are much greater than those due to the area, the discharge coefficient and the real gas correction factor. It is necessary to invoke the properties of the thermal boundary layer to explain these changes, which are found to be greater for gases having a higher specific heat ratio.
机译:的温度对用于表征小音速喷嘴的系数的影响先前的研究(比格内尔和Choi,流量:测量。&仪器厂13(2002)17-22)综述。绝热冷却在喉部气流使待冷却喷嘴的主体,但加热器和温度控制系统允许喷嘴的温度将保持恒定。使用可以在连续模式下操作的气体流动的标准,测量在使用空气,氩气,氮气和二氧化碳的不同温度下由喷嘴系数。喷嘴系数与气体类型和直线与所述喷嘴的所述主体的温度而变化。第一这些变化是通过在氩气的实际气体校正因子的变化,但不用于二氧化碳说明。温度的变化比由于区域,排出系数和实际气体校正因子大得多。有必要调用热边界层的特性来解释这些变化,这被发现是更大的具有较高的比热比的气体。

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