Serial/Series Title

The comparative performance of an aviation engine at normal and high inlet air temperatures (open access)

The comparative performance of an aviation engine at normal and high inlet air temperatures

"This report presents some results obtained during an investigation to determine the effect of high inlet air temperature on the performance of a Liberty 12 aviation engine. The purpose of this investigation was to ascertain, for normal service carburetor adjustments and a fixed ignition advance, the relation between power and temperature for the range of carburetor air temperatures that may be encountered when supercharging to sea level pressure at altitudes of over 20,000 feet and without intercooling when using plain aviation gasoline and mixtures of benzol and gasoline" (p. 409).
Date: February 11, 1927
Creator: Gardiner, Arthur W. & Schey, Oscar W.
System: The UNT Digital Library
Two-Dimensional Subsonic Compressible Flow Past Elliptic Cylinders (open access)

Two-Dimensional Subsonic Compressible Flow Past Elliptic Cylinders

"The method of Poggi is used to calculate, for perfect fluids, the effect of compressibility upon the flow on the surface of an elliptic cylinder at zero angle of attack and with no circulation. The result is expressed in a closed form and represents a rigorous determination of the velocity of the fluid at the surface of the obstacle insofar as the second approximation is concerned. Comparison is made with Hooker's treatment of the same problem according to the method of Janzen and Rayleight and it is found that, for thick elliptic cylinders, the two methods agree very well" (p. 245).
Date: February 11, 1938
Creator: Kaplan, Carl
System: The UNT Digital Library