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SRM Internal Flow Tests and Computational Fluid Dynamic AnalysisAn evaluation of the effect of model inlet air temperature drift during a test run was performed to aid in the decision on the need for and/or the schedule for including heaters in the SRMAFTE. The Sverdrup acceptance test data was used to determine the drift in air temperature during runs over the entire range of delivered flow rates and pressures. The effect of this temperature drift on the model Reynolds number was also calculated. It was concluded from this study that a 2% change in absolute temperature during a test run could be adequately accounted for by the data analysis program. A handout package of these results was prepared and presented to ED35 management.
Document ID
19970014889
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
November 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ERCI/HSV-TR95-02
NASA-CR-203933
NAS 1.26:203933
Accession Number
97N18101
Funding Number(s)
CONTRACT_GRANT: NAS8-39095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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