Air-flow and performance characteristics of engine-stage supercharger of a double-row radial aircraft engine.
2 - Effect of design variables /
Edmund J. Baas and Paul D. Dugan.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Advisory Committee for Aeronautics, [1946].
- Summary
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An investigation has been conducted to determine the effect of the location of the diffuser vanes with respect to the supercharger outlets and the effect of flow conditions at the impeller inlet on the air-flow distribution in the outlets of the engine-state supercharger of an 18-cylinder double-row radial aircraft engine. The standard 13-vane diffuser rotated 180 degrees from its original position and an NACA designed 18-vane diffuser were used to determine the effect of the diffuser-vane location with respect to the supercharger outlets. The 18 vanes of the diffuser correspond to the 18 outlets of the supercharger. The effect of flow conditions at the impeller inlet was investigated by distorting the flow at the inlet and noting the effect in the supercharger outlets. An NACA vaneless diffuser was used in this investigation to eliminate the diffuser-vane effect.
- Note
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Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.
Originally issued as NACA as Memorandum Report E6G25 (August 1946).
NACA Wartime Report E-285.
- Physical Description
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10, [15] p. :
ill. ;
27 cm.
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