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    Results of Tests on Radiators for Aircraft Engines (1920)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Part 1 is to present the results of tests on 56 types of core in a form convenient for use in the study of the performance of and possible improvements in existing designs. Working rules are given by which the data contained in the report may be used, and the most obvious conclusions as to the behavior of cores are summarized. Part 2 presents the results of tests made to determine the pressure necessary to produce water flows up to 50 gallons per minute through an 8-inch square section of radiator core. These data are of special value in evaluating the hydraulic head against which the circulating pump is required to operate.
    Type: NACA-TR-63
    Format: application/pdf
    Location Call Number Expected Availability
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