Theory of cylinder cooling developed previously was further substantiated by data obtained on cylinder from Wright R-1820-G engine; equations presented for average head and barrel temperatures of this cylinder as functions of engine and cooling conditions; these equations are utilized to calculate variation in cylinder temperature with altitude for level flight and climb.
Correlation of cooling data from air-cooled cylinder and several multicylinder engines
Nat Advisory Committee Aeronautics -- Report
1940
5 pages
Report
Englisch
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