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Computing Flows Of Coolants In TurbomachinesCoolant Passage Flow (CPF) computer code developed to predict accurately coolant flow and heat transfer inside turbomachinery cooling passages (either radial or axial blading). Computes flow in one-inlet/one-outlet passage of any shape. Calculates rate of flow of coolant, temperature, pressure, velocity, and heat-transfer coefficients along passage. Integrates one-dimensional momentum and energy equations along defined flow path, taking into account change in area, addition or subtraction of mass, pumping, friction, and transfer of heat. Written in FORTRAN IV.
Document ID
19940000156
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Meitner, P. L.
(Army Propulsion Directorate)
Date Acquired
August 16, 2013
Publication Date
March 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-15180
Accession Number
94B10156
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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