Experimental technique and assessment for measuring the convective heat transfer coefficient from natural ice accretions
Abstract
A 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.
- Publication:
-
Presented at the 33rd Aerospace Sciences Meeting and Exhibit
- Pub Date:
- March 1995
- Bibcode:
- 1995aesc.meet....9M
- Keywords:
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- Aircraft Icing;
- Convective Heat Transfer;
- Ice;
- Ice Formation;
- Metal Surfaces;
- Parallel Flow;
- Wind Tunnel Tests;
- Aluminum;
- Flat Plates;
- Heat Flux;
- Heat Transfer Coefficients;
- Fluid Mechanics and Heat Transfer