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Experimental Technique and Assessment for Measuring the Convective Heat Transfer Coefficient from Natural Ice AccretionsA technique was developed to cast frozen ice shapes that had been grown on a metal surface. This technique was applied to a series of ice shapes that were grown in the NASA Lewis Icing Research Tunnel on flat plates. Nine flat plates, 18 inches square, were obtained from which aluminum castings were made that gave good ice shape characterizations. Test strips taken from these plates were outfitted with heat flux gages, such that when placed in a dry wind tunnel, can be used to experimentally map out the convective heat transfer coefficient in the direction of flow from the roughened surfaces. The effects on the heat transfer coefficient for both parallel and accelerating flow will be studied. The smooth plate model verification baseline data as well as one ice roughened test case are presented.
Document ID
19950016828
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Masiulaniec, K. Cyril
(Toledo Univ. OH., United States)
Vanfossen, G. James, Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Dewitt, Kenneth J.
(Toledo Univ. OH., United States)
Dukhan, Nihad
(Toledo Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-9476
AIAA PAPER 95-0537
NAS 1.15:106864
NASA-TM-106864
Report Number: E-9476
Report Number: AIAA PAPER 95-0537
Report Number: NAS 1.15:106864
Report Number: NASA-TM-106864
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 9, 1995
End Date: January 12, 1995
Accession Number
95N23248
Funding Number(s)
CONTRACT_GRANT: NAG3-72
PROJECT: RTOP 505-68-10
Distribution Limits
Public
Copyright
Public Use Permitted.
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