Effects of inlet air pressure, inlet air temperature, and compression ratio on maximum permissible performance obtained on single cylinder test engine with aircraft engine fuels varying from 87 octane number to 100 octane number with 1 ml of tetraethyl lead per gallon.
Engine performance and knock rating of fuels for high-output aircraft engines
Nat Advisory Committee Aeronautics -- Tech Note
1938
19 pages
14 Supp plates, Bibliography
Article (Journal)
English
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Engine performance and knock rating of fuels for high-output aircraft engines
Engineering Index Backfile | 1938
|Engineering Index Backfile | 1933
Engineering Index Backfile | 1933
|SAE Technical Papers | 1931
|Online Contents | 2003
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