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Nasa Technical Reports Server (ntrs) 19930089348%3a Analysis Of Turbomachine Viscous Losses Affected By Changes In Blade Geometry by Nasa Technical Reports Server (ntrs)

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1NASA Technical Reports Server (NTRS) 19930089348: Analysis Of Turbomachine Viscous Losses Affected By Changes In Blade Geometry

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The effect of changes in blade geometry on the viscous losses in turbomachines is analyzed. The viscous losses can be expressed as a function of three variables: the blade height-to spacing ratio, the solidity, and a blade-height Reynolds number. A method of optimizing the number of blades and the solidity is given. The effect of trailing-edge blockage on blade loss and its effect on the choice of blade number for a particular design are also discussed.

“NASA Technical Reports Server (NTRS) 19930089348: Analysis Of Turbomachine Viscous Losses Affected By Changes In Blade Geometry” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19930089348: Analysis Of Turbomachine Viscous Losses Affected By Changes In Blade Geometry
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  • Language: English

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