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Sensitivity of SAE Total Pressure Intake Distortion Descriptors to Pressure Fluctuations at the Engine-Intake Interface Plane Airbus

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Funes Sebastian, Funes Sebastian, author.
Conference Name:
Aerospace Technology Conference & Exposition (2011-10-18 : Toulouse, France)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2011
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
2011-01-2544
Access Restriction:
Restricted for use by site license

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