Publication Date:
2019-07-13
Description:
A technique for extracting the in-stall pumping characteristics for an axial flow compressor operating in an engine system environment is developed. The technique utilizes a Hybrid computer simulation of the compressor momentum equation into which actual transient data are used to provide all terms but the desired compressor characteristic. The compressor force characteristic as a function of corrected flow and speed result from the computation. The critical problem of data filtering is addressed. Results for a compressor operating in a turbofan engine are presented and comparison is made with the conventional compressor map. The relationship of the compressor surge characteristic with its rotating stall characteristic is explored. Initial interpretation of the measured results is presented.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-83639
,
E-2082
,
NAS 1.15:83639
,
Joint Propulsion Conf.; Jun 11, 1983 - Jun 13, 1983
Format:
application/pdf
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