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Estimating turbine limit loadA method for estimating turbine limit-load pressure ratio from turbine map information is presented and demonstrated. It is based on a mean line analysis at the last-rotor exit. The required map information includes choke flow rate at all speeds as well as pressure ratio and efficiency at the onset of choke at design speed. One- and two-stage turbines are analyzed to compare the results with those from a more rigorous off-design flow analysis and to show the sensitivities of the computed limit-load pressure ratios to changes in the key assumptions.
Document ID
19930016694
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glassman, Arthur J.
(Toledo Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-191105
E-7705
NAS 1.26:191105
Report Number: NASA-CR-191105
Report Number: E-7705
Report Number: NAS 1.26:191105
Accession Number
93N25883
Funding Number(s)
PROJECT: RTOP 505-69-50
CONTRACT_GRANT: NAG3-1165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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