Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder
Description:
Several methods of predicting the compressible-flow pressure loss across a baffled aircraft-engine cylinder were analytically related and were experimentally investigated on a typical air-cooled aircraft-engine cylinder. Tests with and without heat transfer covered a wide range of cooling-air flows and simulated altitudes from sea level to 40,000 feet. Both the analysis and the test results showed that the method based on the density determined by the static pressure and the stagnation temperat…
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Date:
October 9, 1945
Creator:
Neustein, Joseph & Schafer, Louis J., Jr.
Item Type:
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Partner:
UNT Libraries Government Documents Department