Serial/Series Title

Month

Effect of spark-timing regularity on the knock of engine performance (open access)

Effect of spark-timing regularity on the knock of engine performance

Tests on a high-speed single-cylinder engine are described. The regularity of the spark timing was varied by driving the timer from different engine shafts. A simple and reasonably accurate method of determining the spark timing is described. The results show that irregular spark timing may cause large errors in tests of the knocking properties of fuels. For the engine tested, it was found that a change of one crankshaft degree in spark restart was equivalent to an 0.85 inch Hg change in allowable inlet pressure.
Date: May 1938
Creator: Biermann, Arnold E.
System: The UNT Digital Library
The increase in frictional resistance caused by various types of rivet heads as determined by tests of planing surfaces (open access)

The increase in frictional resistance caused by various types of rivet heads as determined by tests of planing surfaces

"The increase in the frictional resistance of a surface caused by the presence of rivet heads was determined by towing four planing surfaces of the same dimensions. One surface was smooth and represented a surface without rivet heads or one with perfectly flush countersunk rivets. The other three surfaces were each fitted with the same number of full-size rivet heads but of a different type arranged in the same pattern on each surface" (p. 1).
Date: May 1938
Creator: Truscott, Starr & Parkinson, J. B.
System: The UNT Digital Library
The effect of air-passage length on the optimum fin spacing for maximum cooling (open access)

The effect of air-passage length on the optimum fin spacing for maximum cooling

The effect on cooling of baffle length with optimum cylinder finning is discussed. Results from tests of several streamlined cylinders are given. It is shown that by employing several baffles the cooling can be increased several times.
Date: May 1938
Creator: Brevoort, Maurice J.
System: The UNT Digital Library
Wind-Tunnel Tests of a Clark Y Wing Having Split Flaps With Gaps (open access)

Wind-Tunnel Tests of a Clark Y Wing Having Split Flaps With Gaps

"Tests were made of the Clark Y wing having split flaps with a gap between the flap and the lower surface of the wing. Lift, drag, and pitching moments were measured for the wing with three different sizes of flap. It was found that any gap between the flap and the wing reduced the lift, the drag, and the pitching moments, but that the center-of-pressure movement and the ratio of lift to drag were little affected" (p. 1).
Date: May 1938
Creator: Wenzinger, Carl J.
System: The UNT Digital Library