Performance of Two-Stage Turbosupercharger Using Mixed-Flow Impellers

Abstract

The NACA has investigated the performance of a two-stage turbosupercharger incorporating mixed-flow impellers. Two complete superchargers were tested, the second being the same as the first except for modified vanes in the interstage passage and a somewhat different first-stage diffuser shape. At the maximum pressure ratio of 2.91 the peak efficiency of the modified supercharger was 78% at a corrected volume flow of 115 cubic feet per second. The modified supercharger had a maximum efficiency of slightly above 82%, an increase of 3 points above that of the original compressor. At the highest common pressure ratio of 2.6, the modified supercharger reached a peak efficiency of 80% and the original supercharger, 74%. The characteristic curves of both units were fairly flat, which indicated good performance for a wide range of speeds and air flows.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1942
Accession Number
ADA801307

Entities

People

  • Julia A. King
  • Oscar W. Schey

Organizations

  • Glenn Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautics
  • Air Flow
  • Aircrafts
  • Centrifugal Compressors
  • Compressors
  • Diameters
  • Diffusers
  • Efficiency
  • Flow
  • Heat Transfer
  • Impellers
  • Measurement
  • Navy
  • Sea Level
  • Standards
  • Superchargers
  • Turbosuperchargers

Readers

  • Aerodynamics.
  • Mathematics or Statistics