Add to ORKGAn investigation was conducted to correlate the knock limited performance of flight and single-cylinder engines under a variety of operating conditions
Tests made on a Curtiss D-12 engine in the Altitude Laboratory at the Bureau of Standards show the f...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
Report presents the design of radiators, spark plugs and test equipment used to test the performance...
Variable charge-air flow, cooling-air pressure drop, and fuel-air ration investigations were conduct...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
The temperature distribution of a two-row radial engine in a twin-engine airplane has been investiga...
One of the most important properties of aviation fuels for spark-ignition engines is their knock rat...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
The knock-limited performance of blends of 0,50; and 100 percent by volume of 2,2,3-trimethylpentane...
Given here are the results of tests made to determine the effect of fuel consumption on the cylinder...
A continuous 50-hour test was conducted to determine the effect of maximum cruise-power operation at...
Presented here are the results of performance tests made with a single-cylinder, four stroke cycle, ...
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-...
Report presents the results of performance tests of a single-cylinder 4-stroke-cycle compression-ign...
Tests made on a Curtiss D-12 engine in the Altitude Laboratory at the Bureau of Standards show the f...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
Report presents the design of radiators, spark plugs and test equipment used to test the performance...
Variable charge-air flow, cooling-air pressure drop, and fuel-air ration investigations were conduct...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
The temperature distribution of a two-row radial engine in a twin-engine airplane has been investiga...
One of the most important properties of aviation fuels for spark-ignition engines is their knock rat...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
The knock-limited performance of blends of 0,50; and 100 percent by volume of 2,2,3-trimethylpentane...
Given here are the results of tests made to determine the effect of fuel consumption on the cylinder...
A continuous 50-hour test was conducted to determine the effect of maximum cruise-power operation at...
Presented here are the results of performance tests made with a single-cylinder, four stroke cycle, ...
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-...
Report presents the results of performance tests of a single-cylinder 4-stroke-cycle compression-ign...
Tests made on a Curtiss D-12 engine in the Altitude Laboratory at the Bureau of Standards show the f...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
Report presents the design of radiators, spark plugs and test equipment used to test the performance...