Orifice Mass Flow Calculation in NASA's W-8 Single Stage Axial Compressor Facility

Bozak, Richard F

关键词: ORIFICE FLOW;    MASS FLOW;    DISCHARGE COEFFICIENT;    HUMIDITY;    INLET PRESSURE;    TURBOCOMPRESSORS;    STATIC PRESSURE;    INLET FLOW;    TURBOFANS;    ORIFICES;    ROTORS;   

RP-ID  :  NASA/TM-2018-219762,E-19474,GRC-E-DAA-TN50467

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来源: NASA Technical Reports Server

【 摘 要 】

Updates to the orifice mass flow calculation for the W-8 Single Stage Axial Compressor Facility at NASA Glenn Research Center are provided to include the effect of humidity and incorporate ISO 5167. A methodology for including the effect of humidity into the inlet orifice mass flow calculation is provided. Orifice mass flow calculations provided by ASME PTC-19.5-2004, ASME MFC-3M-2004, ASME Fluid Meters, and ISO 5167 are compared for W-8's atmospheric inlet orifice plate. Differences in expansion factor and discharge coefficient given by these standards give a variation of about +/- 75% mass flow except for a few cases. A comparison of the calculations with an inlet static pressure mass flow correlation and a fan exit mass flow integration using test data from a 2017 turbofan rotor test in W-8 show good agreement between the inlet static pressure mass flow correlation, ISO 5167, and ASME Fluid Meters. While W-8's atmospheric inlet orifice plate violates the pipe diameter limit defined by each of the standards, the ISO 5167 is chosen to be the primary orifice mass flow calculation to use in the W-8 facility.