Abstract
The objective of this work is to provide a correlation between the heat transfer coefficient and the Nusselt Number with the flow Reynolds number for a truncated cylindrical probe in cross-flow, a configuration that has not previously been well defined. In the experiment, thermally stabilized, dry air was discharged into the test section across a heated probe that was instrumented with thermocouples and exhausted to atmosphere. Experimental data were recorded for several run conditions. A correlation between the probe heat transfer coefficient and the Reynolds number was developed with a calculated uncertainty of 1.24%.
Keywords::
Acknowledgments
The authors wish to thank Joel Davenport for his support in the laboratory and Sabrina Hurlock for her help with uncertainty analysis.
FUNDING
This work was partially funded by United States Air Force under contract FA9101-06-D-0001/0016.