Sensitivity of SAE Total Pressure Intake Distortion Descriptors to Pressure Fluctuations at the Engine-Intake Interface Plane 2011-01-2544
A methodology to evaluate the sensitivity of total pressure intake distortion descriptors defined by SAE ARP 1420 to individual pressure fluctuations in the Aerodynamic Interface Plane -AIP- has been developed. Individual pressure fluctuations were simulated as a white noise using a random number generator with a Gaussian distribution of known standard deviation. Monte Carlo experiments were performed perturbing different steady total pressure patterns on the AIP with random signals of different RMS values. Instantaneous distortion descriptors were calculated and statistically characterized. General correlations were obtained applying maximum value statistics to relate the maximum expected distortion increment to the RMS of the individual pressure fluctuations, the mean total pressure on the AIP and the number of samples.
Citation: Funes Sebastian, D., "Sensitivity of SAE Total Pressure Intake Distortion Descriptors to Pressure Fluctuations at the Engine-Intake Interface Plane," SAE Technical Paper 2011-01-2544, 2011, https://doi.org/10.4271/2011-01-2544. Download Citation
Author(s):
David Ernesto Funes Sebastian
Affiliated:
Airbus
Pages: 13
Event:
Aerospace Technology Conference and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Pressure
Statistical analysis
Logistics
Aerodynamics
Noise
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