10 REPORT NO. 587 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS maximum heat transfer for a given weight velocity will the 0.166, the 0.137, and the 0.112 cyHnders is ap- give maximum heat transfer for a given power. proximately constant. Figure 14 shows curves similar to figure 13 in which Further… … Pt,, horsepower per inch of cylinder length KniURE 14.—Variation of average wall heat-transfer coefficient with total power, Ph. Specific weight of the air, 0.0717 pound per cubic foot. exit passage of the jacket is included in calculating the required power. As previously stated, the power lost at…
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