Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines (1933)
NASA Technical Reports Server (NTRS) · leaf 7
discharge at varying length-diameter ratio of the 0.003- lb.persq.cn. inch discharge orifice. Atmospherlo chamber air density. Plain stem The explanation of irregularities in the penetration and coefficient of discharge curves is found in an Injection pressure,' analysis of the flow through the… … Reynolds Number which resulted in a different condition of flow within Florae 9.—Coefficient of discharge at varying Heynolds Number the nozzle than with the tests reported herein. The orifice the jet is given a spiral motion and a tendency difference in the flow conditions may be seen by com- to…
NASA Technical Reports Server (NTRS)
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