NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Computer program for analysis of split-Stirling-cycle cryogenic coolersA computer program for predicting the detailed thermodynamic performance of split-Stirling-cycle refrigerators has been developed. The mathematical model includes the refrigerator cold head, free-displacer/regenerator, gas transfer line, and provision for modeling a mechanical or thermal compressor. To allow for dynamic processes (such as aerodynamic friction and heat transfer) temperature, pressure, and mass flow rate are varied by sub-dividing the refrigerator into an appropriate number of fluid and structural control volumes. Of special importance to modeling of cryogenic coolers is the inclusion of real gas properties, and allowance for variation of thermo-physical properties such as thermal conductivities, specific heats and viscosities, with temperature and/or pressure. The resulting model, therefore, comprehensively simulates the split-cycle cooler both spatially and temporally by reflecting the effects of dynamic processes and real material properties.
Document ID
19840007276
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, M. T.
(Hughes Aircraft Co. El Segundo, CA, United States)
Russo, S. C.
(Hughes Aircraft Co. El Segundo, CA, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1983
Publication Information
Publication: NASA. Goddard Space Flight Center Refrig. for for Cryogenic Sensors
Subject Category
Engineering (General)
Accession Number
84N15344
Funding Number(s)
CONTRACT_GRANT: F33615-79-C-3402
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available