The effect of internal cooling on the knock-limited performance of an-f-28 fuel was investigated in a CFR engine, and the following internal coolants were used: (1) water, (2), methyl alcohol-water mixture, (3) ammonia-methyl alcohol-water mixture, (4) monomethylamine-water mixture, (5) dimethylamine-water mixture, and (6) trimethylamine-water mixture. Tests were run at inlet-air temperatures of 150 degrees and 250 degrees F. to indicate the temperature sensitivity of the internal-coolant solutions
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...
The knock-limited performance of nine fuels, comprising isolated members of four classes of hydrocar...
The effect of internal cooling on the knock-limited performance of an-f-28 fuel was investigated in ...
Engine tests, together with estimates made at Langley Memorial Aeronautical Laboratory, indicate tha...
An investigation of the antiknock effectiveness of various additive-water solutions when used as int...
A Wright GR-1820-G200 cylinder was tested over a wide range of fuel-air ratios at maximum permissibl...
Preignition-limited performance data were obtained on a supercharged CFR engine at two sets of opera...
An investigation was conducted to correlate the knock limited performance of flight and single-cylin...
A knock-limited performance investigation was conducted on blends of triptane and 28-P fuel with a 1...
Six 100-octane and two 87-octane aviation engine fuels were tested in a modified C.F.R. variable-com...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
An investigation was conducted to determine the effect of a coolant solution of 25 percent ethyl alc...
To determine the effect of piston-head temperature on knock-limited power. Tests were made in a supe...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
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...
The knock-limited performance of nine fuels, comprising isolated members of four classes of hydrocar...
The effect of internal cooling on the knock-limited performance of an-f-28 fuel was investigated in ...
Engine tests, together with estimates made at Langley Memorial Aeronautical Laboratory, indicate tha...
An investigation of the antiknock effectiveness of various additive-water solutions when used as int...
A Wright GR-1820-G200 cylinder was tested over a wide range of fuel-air ratios at maximum permissibl...
Preignition-limited performance data were obtained on a supercharged CFR engine at two sets of opera...
An investigation was conducted to correlate the knock limited performance of flight and single-cylin...
A knock-limited performance investigation was conducted on blends of triptane and 28-P fuel with a 1...
Six 100-octane and two 87-octane aviation engine fuels were tested in a modified C.F.R. variable-com...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
An investigation was conducted to determine the effect of a coolant solution of 25 percent ethyl alc...
To determine the effect of piston-head temperature on knock-limited power. Tests were made in a supe...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
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...
The knock-limited performance of nine fuels, comprising isolated members of four classes of hydrocar...