The Effect of Nozzle Design and Operating Conditions on the Atomization and Distribution of Fuel Sprays (1933)
NASA Technical Reports Server (NTRS) · leaf 9
REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS (») Plain nozzle, 0.020-inch orifice. Effective injection pressure—4,120 lb. (•) Plain nozzle, 0.020-inch orifice. Effective injection pressure— 4,120 lb. per per sq. in. Position on record—A-2 sq. in. Position on record—A-14 … Reproduced from best available copy.
NASA Technical Reports Server (NTRS)
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