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  • Numerical Analysis; Research and Support Facilities (Air); Fluid Mechanics and Thermodynamics  (2)
  • 2015-2019  (2)
  • 1995-1999
  • 2015  (2)
  • 1
    Publication Date: 2019-07-13
    Description: A numerical, and experimental investigation to study the effects of flow distortion on a Mass Flow Plug (MFP) used to control and measure mass-flow during an inlet test has been conducted. The MFP was first calibrated using the WIND-US flow solver for uniform (undistorted) inflow conditions. These results are shown to compare favorably with an experimental calibration under similar conditions. The effects of distortion were investigated by imposing distorted flow conditions taken from an actual inlet test to the inflow plane of the numerical simulation. The computational fluid dynamic (CFD) based distortion study only showed the general trend in mass flow rate. The study used only total pressure as the upstream boundary condition, which was not enough to define the flow. A better simulation requires knowledge of the turbulence structure and a specific distortion pattern over a range of plug positions. It is recommended that future distortion studies utilize a rake with at least the same amount of pitot tubes as the AIP rake.
    Keywords: Numerical Analysis; Research and Support Facilities (Air); Fluid Mechanics and Thermodynamics
    Type: GRC-E-DAA-TN24118 , AIAA Propulsion and Energy Conference; Jul 27, 2015 - Jul 29, 2015; Orlando, FL; United States
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: A simple control volume model has been developed to calculate the discharge coefficient through a mass flow plug (MFP) and validated with a calibration experiment. The maximum error of the model within the operating region of the MFP is 0.54%. The control volume analysis developed work is comprised of a sequence of flow calculations through the MFP. The model uses the MFP geometry and operating pressure and temperature to couple continuity, momentum, energy, an equation of state, and wall shear. The discharge coefficient calculation also includes the effects of boundary layer growth, including the reduction in cross-sectional flow area as characterized by the boundary layer displacement thickness. The last calculation in the sequence uses an integral method to calculate the growth of the boundary layer, from which the displacement thickness is then determined. The result of these successive calculations is an accurate one-dimension model of the velocity, pressure, and temperature through the MFP. For comparison, a computational fluid dynamic (CFD) calibration is shown, which when compared to the presented numerical model, had a lower accuracy with a maximum error of 1.35% in addition to being slower by a factor of 100."
    Keywords: Numerical Analysis; Research and Support Facilities (Air); Fluid Mechanics and Thermodynamics
    Type: GRC-E-DAA-TN24115 , International Energy Conversion Engineering Conference (IECEC 2015); Jul 27, 2015 - Jul 29, 2015; Orlando, FL; United States
    Format: application/pdf
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