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Vapor Flow Patterns During a Start-Up Transient in Heat PipesThe vapor flow patterns in heat pipes are examined during the start-up transient phase. The vapor core is modelled as a channel flow using a two dimensional compressible flow model. A nonlinear filtering technique is used as a post process to eliminate the non-physical oscillations of the flow variables. For high-input heat flux, multiple shock reflections are observed in the evaporation region. The reflections cause a reverse flow in the evaporation and circulations in the adiabatic region. Furthermore, each shock reflection causes a significant increase in the local pressure and a large pressure drop along the heat pipe.
Document ID
19980027096
Acquisition Source
Armstrong Flight Research Center
Document Type
Contractor Report (CR)
Authors
Issacci, F.
(California Univ. Los Angeles, CA United States)
Ghoniem, N, M.
(California Univ. Los Angeles, CA United States)
Catton, I.
(California Univ. Los Angeles, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-204367
NAS 1.26:204367
Report Number: NASA-CR-204367
Report Number: NAS 1.26:204367
Funding Number(s)
CONTRACT_GRANT: NCC2-374
CONTRACT_GRANT: NAG3-899
CONTRACT_GRANT: DE-FG03-86ER-52126
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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