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Investigation of flow coefficient of circular, square, and elliptical orifices at high pressure ratios

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:25:56Z
date available2017-09-04T16:25:56Z
date copyright01/01/1949
date issued1949
identifier otherTYZTYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/89197
description abstractINTRODUCTION
The introduction of a gas or a vapor into an air stream for Purposes of heating or cooling the air stream may be easily accomplished by the use of a high-velocity jet directed perpendicularly to the air stream, as reported in reference 1. In order to evaluate the heating or cooling effect of such a Jet, knowledge of the mass air flow of the Jet or, more fundamentally, the discharge coefficient of the orifice from which the Jet is issuing is essential. In addition to the effects of Jet Reynolds number and orifice shape on the discharge coefficient, the Jet pressure ratio and the interaction of the air stream and the Jet must be considered.
An investigation to determine the orifice-discharge coefficient of a high-velocity air Jet directed perpendicularly to an air stream was undertaken in a 2- by 20-1nch duct tunnel at the NACA Lewis laboratory. The discharge coefficients of circular, square, and elliptical orifices were determined at tunnel-air velocities of 160, 2275, and 380 feet per second for several Jet (orifice) areas, A range of pressure ratios from 1.15 to 3.2, and a Jet total temperature of approximately 400° F.
languageEnglish
titleNACA-TN-1947num
titleInvestigation of flow coefficient of circular, square, and elliptical orifices at high pressure ratiosen
typestandard
page28
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1949
contenttypefulltext
subject keywordsAIR
subject keywordsFLOW
subject keywordsJETS
subject keywordsNUMBER
subject keywordsORIFICES
subject keywordsREYNOLDS


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