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NACA-TM-722

Guide vanes for deflecting fluid currents with small loss of energy

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1933

Abstract: The transverse momentum of the deflected air stream to be absorbed is divided between the intermediate and outside walls, so that the pressure increase on each wall is much smaller and the danger of separation is diminished. The formation of secondary vortices is also diminished. By taking as the basis profiles with high c(sub a), such as have proved practically favorable, it is not possible to find a satisfactory form of grid simply on the assumption that the flow is potential. The requirements called for the most uniform possible velocity distribution behind the bend and the smallest possible losses.
URI: https://yse.yabesh.ir/std/handle/yse/110622
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    NACA-TM-722

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:47:18Z
date available2017-09-04T16:47:18Z
date copyright01/01/1933
date issued1933
identifier otherBTONEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/110622
description abstractThe transverse momentum of the deflected air stream to be absorbed is divided between the intermediate and outside walls, so that the pressure increase on each wall is much smaller and the danger of separation is diminished. The formation of secondary vortices is also diminished. By taking as the basis profiles with high c(sub a), such as have proved practically favorable, it is not possible to find a satisfactory form of grid simply on the assumption that the flow is potential. The requirements called for the most uniform possible velocity distribution behind the bend and the smallest possible losses.
languageEnglish
titleNACA-TM-722num
titleGuide vanes for deflecting fluid currents with small loss of energyen
typestandard
page44
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1933
contenttypefulltext
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