NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Emittance Measurements for a Thin Liquid Sheet FlowThe Liquid Sheet Radiator (LSR) is an external flow radiator that uses a triangular-shaped flowing liquid sheet as the radiating surface. It has potentially much lower mass than solid wall radiators such as pumped loop and heat pipe radiators, along with being nearly immune to micrometeoroid penetration. The LSR has an added advantage of simplicity. Surface tension causes a thin (100-300 microns) liquid sheet to coalesce to a point, causing the sheet flow to have a triangular shape. Such a triangular sheet is desirable since it allows for simple collection of the flow at a single point. A major problem for all external flow radiators is the requirement that the working fluid be of very low (approx. 10(sup -8) torr) vapor pressure to keep evaporative losses low. As a result, working fluids are limited to certain oils (such as used in diffusion pumps) for low temperatures (300-400 K) and liquid metals for higher temperatures. Previous research on the LSR has been directed at understanding the fluid mechanics of thin sheet flows and assessing the stability of such flows, especially with regard to the formation of holes in the sheet. Taylor studied extensively the stability of thin liquid sheets both theoretically and experimentally. He showed that thin sheets in a vacuum are stable. The latest research has been directed at determining the emittance of thin sheet flows. The emittance was calculated from spectral transmittance data for the Dow Corning 705 silicone oil. By experimentally setting up a sheet flow, the emittance was also determined as a function of measurable quantities, most importantly, the temperature drop between the top of the sheet and the temperature at the coalescence point of the sheet. Temperature fluctuations upstream of the liquid sheet were a potential problem in the analysis and were investigated.
Document ID
19970023379
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Englehart, Amy N.
(Cleveland State Univ. Cleveland, OH United States)
McConley, Marc W.
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Chubb, Donald L.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Publication Information
Publication: Journal of Thermophysics and Heat Transfer
Publisher: American Institute of Aeronautics and Astronautics
Volume: 10
Issue: 3
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:204653
AIAA Paper 96-0237
NASA-CR-204653
Report Number: NAS 1.26:204653
Report Number: AIAA Paper 96-0237
Report Number: NASA-CR-204653
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 15, 1996
End Date: January 18, 1996
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
97N23721
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available