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An improved design method and experimental performance of two dimensional curved wall diffusers

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:50:13Z
date available2017-09-04T15:50:13Z
date copyright01/01/1972
date issued1972
identifier otherQGLNGEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/53313
description abstractA computer design program was developed to incorporate the suction slots in solving the potential flow equations with prescribed boundary conditions. Using the contour generated from this program two Griffith diffusers were tested having area ratios AR = 3 and 4. The inlet Reynolds number ranged from 600,000 to 7 million. It was found that the slot suction required for metastable operation depends on the sidewall suction applied. Values of slot suction of 8% of the inlet flow rate was required for AR = 4 with metastable condition, provided that enough sidewall suction was applied. For AR = 3, the values of slot suction was about 25% lower than those required for AR = 4. For nearly all unseparated test runs, the effectiveness was 100% and the exit flow was uniform. In addition to the Griffith diffusers, dump and cusp diffusers of comparable area ratios were built and tested. The results obtained from these diffusers were compared with those of the Griffith diffusers. Flow separation occurred in all test runs with the dump and cusp diffusers.
languageEnglish
titleNASA-CR-121024num
titleAn improved design method and experimental performance of two dimensional curved wall diffusersen
typestandard
page77
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1972
contenttypefulltext
subject keywordsBOUNDARY CONDITIONS
subject keywordsBOUNDARY LAYER CONTROL
subject keywordsCOMPUTER AIDED DESIGN
subject keywordsDIFFUSERS
subject keywordsFLOW VELOCITY
subject keywordsSUCTION
subject keywordsWALLS


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