NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Current status of liquid sheet radiator researchInitial research on the external flow, low mass liquid sheet radiator (LSR), has been concentrated on understanding its fluid mechanics. The surface tension forces acting at the edges of the sheet produce a triangular planform for the radiating surface of width, W, and length, L. It has been experimentally verified that (exp L)/W agrees with the theoretical result, L/W = (We/8)exp 1/2, where We is the Weber number. Instability can cause holes to form in regions of large curvature such as where the edge cylinders join the sheet of thickness, tau. The W/tau limit that will cause hole formation with subsequent destruction of the sheet has yet to be reached experimentally. Although experimental measurements of sheet emissivity have not yet been performed because of limited program scope, calculations of the emissivity and sheet lifetime is determined by evaporation losses were made for two silicon based oils; Dow Corning 705 and Me(sub 2). Emissivities greater than 0.75 are calculated for tau greater than or equal to 200 microns for both oils. Lifetimes for Me(sub 2) are much longer than lifetimes for 705. Therefore, Me(sub 2) is the more attractive working fluid for higher temperatures (T greater than or equal to 400 K).
Document ID
19930004962
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chubb, Donald L.
(NASA Lewis Research Center Cleveland, OH, United States)
Calfo, Frederick D.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcmaster, Matthew S.
(Toledo Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:105764
NASA-TM-105764
E-7181
Report Number: NAS 1.15:105764
Report Number: NASA-TM-105764
Report Number: E-7181
Meeting Information
Meeting: International Conference on Aerospace Heat Exchanger Technology
Location: Palo Alto, CA
Country: United States
Start Date: February 15, 1993
End Date: February 17, 1993
Sponsors: AIAA, ASME
Accession Number
93N14150
Funding Number(s)
PROJECT: RTOP 506-41-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available