NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The induction of water to the inlet air as a means of internal cooling in aircraft-engine cylindersReport presents the results of investigations conducted on a full-scale air-cooled aircraft-engine cylinder of 202-cubic inch displacement to determine the effects of internal cooling by water induction on the maximum permissible power and output of an internal-combustion engine. For a range of fuel-air and water-fuel ratios, the engine inlet pressure was increased until knock was detected aurally, the power was then decreased 7 percent holding the ratios constant. The data indicated that water was a very effective internal coolant, permitting large increases in engine power as limited by either knock or by cylinder temperatures.
Document ID
19930091835
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rothrock, Addison M
Krsek, Alois, Jr
Jones, Anthony W
Date Acquired
September 6, 2013
Publication Date
January 1, 1943
Report/Patent Number
NACA-TR-756
Accession Number
93R21125
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available