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Non-dimensional Performance

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Propulsion and Power
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Abstract

D3 Non-Dimensional Performance We illustrate that if the velocity triangles for a compressor, run to two different conditions, have the same angles and Mach numbers, then the non-dimensional parameters (speed, pressure ratio, temperature ratio, etc.) will also be the same. Without resorting to higher mathematics, this method is extended to cover whole engine parameters such as fuel flow, thrust and power. We show how to correct the non-dimensional parameters to standard conditions using exponents for δ (P/PISA) and Θ (T/TISA) and the use of the cycle model to derive the exponent values for each parameter including humidity and “real engine” effects.

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References

  1. Roberts, S.K.: Effects of Fluid Properties on the Aerodynamic Performance of Turbomachinery for Semi-Closed Cycle Gas Turbine Engines Using O2/CO2 Combustion. Master Thesis 2001 Ottawa-Carleton Institute for Mechanical and Aerospace Engineering (2001)

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  3. Volponi A.J.: Gas Turbine Parameter Corrections. ASME Paper 98-GT-947 (1998)

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  4. Kurzke, J.: Model Based Gas Turbine Parameter Corrections ASME GT2003-38234 (2003)

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Correspondence to Joachim Kurzke .

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Kurzke, J., Halliwell, I. (2018). Non-dimensional Performance. In: Propulsion and Power. Springer, Cham. https://doi.org/10.1007/978-3-319-75979-1_16

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  • DOI: https://doi.org/10.1007/978-3-319-75979-1_16

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-75977-7

  • Online ISBN: 978-3-319-75979-1

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