On Flow Stagnation in a Tube RadiatorAn analysis of the physical process for occurrence of flow stagnation in a space tube-radiator is performed and the mechanism and mathematic description for the flow stagnation are presented. Two causes for pressure drop unbalance between tubes of the radiator are identified: non-uniform cooling environment and different local flow resistances between the tubes. This analysis provides a theoretical basis for experimental simulations of the flow stagnation in a ground-based lab as well as two suggested methods to experimentally simulate flow stagnation. Criteria for the flow stagnation, depending on the viscosity data regressive polynomial, are derived from the extreme condition of the pressure drop in colder tubes. A preliminary numerical calculation is conducted for a space tube-radiator model which confirms the physical and mathematical analyses. The prediction by the criteria for flow stagnation in the tube-radiator model coincides with the numerical calculation result.
Document ID
20080012608
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Motil, Brian (NASA Glenn Research Center Cleveland, OH, United States)
Chao, David F. (NASA Glenn Research Center Cleveland, OH, United States)
Sankovic, John M. (NASA Glenn Research Center Cleveland, OH, United States)
Zhang, Nengli (Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2007
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2008-825Report Number: AIAA Paper 2008-825
Meeting Information
Meeting: AIAA Conference
Location: Reno, NV
Country: United States
Start Date: January 7, 2008
End Date: January 10, 2008
Sponsors: American Inst. of Aeronautics and Astronautics