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  • 1
    Publication Date: 2019-07-20
    Description: The thermal analysis of a heat exchanger for heating air to temperatures on the order of 3000 C for use in NASA's high temperature wind tunnel is presented. It was ascertained that an externally finned shell-and-tube type of heat exchanger with counterflow could be considered for this application. The methods of estimating the convective heat transfer coefficients are outlined in this report. As a part of thermal design the required size of heat exchanger was predicted. As a result of the extreme length required (approx. = 1/2 km), it was determined that a conventional heat exchanger may not be the most suitable tool for this application.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-CR-179868 , NAS 1.26:179868
    Format: application/pdf
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