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Two phase choke flow in tubes with very large L/D

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:44:09Z
date available2017-09-04T16:44:09Z
date copyright01/01/1977
date issued1977
identifier otherVWHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/107472
description abstractData were obtained for two phase and gaseous choked flow nitrogen in a long constant area duct of 16200 L/D with a diverging diffuser attached to the exit. Flow rate data were taken along five isotherms (reduced temperature of 0.81, 0.96, 1.06, 1.12, and 2.34) for reduced pressures to 3. The flow rate data were mapped in the usual manner using stagnation conditions at the inlet mixing chamber upstream of the entrance length. The results are predictable by a two phase homogeneous equilibrium choking flow model which includes wall friction. A simplified theory which in essence decouples the long tube region from the high acceleration choking region also appears to predict the data resonably well, but about 15 percent low.
languageEnglish
titleNASA-TM-73726num
titleTwo phase choke flow in tubes with very large L/Den
typestandard
page23
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1977
contenttypefulltext
subject keywordsDIFFUSERS
subject keywordsFLOW VELOCITY
subject keywordsISOTHERMS
subject keywordsNITROGEN
subject keywordsPIPE FLOW
subject keywordsPRESSURE
subject keywordsTWO PHASE FLOW


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