Add to ORKGVariable charge-air flow, cooling-air pressure drop, and fuel-air ration investigations were conducted to determine the cooling characteristics of a full-scale air-cooled single cylinder on a CUE setup. The data are compared with similar data that were available for the same model multicylinder engine tested in flight in a four-engine airplane. The cylinder-head cooling correlations were the same for both the single-cylinder and the flight engine. The cooling correlations for the barrels differed slightly in that the barrel of the single-cylinder engine runs cooler than the barrel of te flight engine for the same head temperatures and engine conditions
Flight tests of a Grumman Scout (XSF-2) airplane fitted with a Pratt & Whitney 1535 supercharged eng...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
An analysis based on forced-convection heat-transfer theory, similar to the analysis presented for a...
The cooling characteristics of three R-1830-94 engines, two of which were mounted in a test stand an...
Variable charge-air flow, cooling-air pressure drop, and fuel-air ration investigations were conduct...
Data obtained from an extensive investigation of the cooling characteristics of four multicylinder, ...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
An investigation of the cooling of an 18-cylinder, twin-row, radial, air-cooled engine in a high-per...
Theoretical investigations have shown that, because air is compressible, the pressure-drop requireme...
Theoretical investigations have shown that, because air is compressible, the pressure-drop requireme...
The temperature distribution of a two-row radial engine in a twin-engine airplane has been investiga...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-...
An investigation was conducted to determine the coolant-flow\ud distribution, the cylinder temperatu...
Data for a liquid-cooled engine with a displacement volume of 1710 cubic inches were analyzed to det...
Flight tests of a Grumman Scout (XSF-2) airplane fitted with a Pratt & Whitney 1535 supercharged eng...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
An analysis based on forced-convection heat-transfer theory, similar to the analysis presented for a...
The cooling characteristics of three R-1830-94 engines, two of which were mounted in a test stand an...
Variable charge-air flow, cooling-air pressure drop, and fuel-air ration investigations were conduct...
Data obtained from an extensive investigation of the cooling characteristics of four multicylinder, ...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
An investigation of the cooling of an 18-cylinder, twin-row, radial, air-cooled engine in a high-per...
Theoretical investigations have shown that, because air is compressible, the pressure-drop requireme...
Theoretical investigations have shown that, because air is compressible, the pressure-drop requireme...
The temperature distribution of a two-row radial engine in a twin-engine airplane has been investiga...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-...
An investigation was conducted to determine the coolant-flow\ud distribution, the cylinder temperatu...
Data for a liquid-cooled engine with a displacement volume of 1710 cubic inches were analyzed to det...
Flight tests of a Grumman Scout (XSF-2) airplane fitted with a Pratt & Whitney 1535 supercharged eng...
The theory of engine-cylinder cooling developed in a previous report was further substantiated by da...
An analysis based on forced-convection heat-transfer theory, similar to the analysis presented for a...