Item Details

Analytical Study of Effect of Casing Treatment on Performance of a Multistage Compressor

by Roger W. Snyder and Robert J. Blade
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972.
Language
English
Series
NASA Technical Note
Summary
The simulation was based on individual stage pressure and efficiency maps. These maps were modified to account for casing treatment effects on the individual stage characteristics. The individual stage maps effects on overall compressor performance were observed. The results show that to improve the performance of the compressor in its normal operating range, casing treatment of the rear stages is required.
Description
24 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Lewis Research Center.
  • Cover title.
  • Bibliography: p. 14.
Series Statement
NASA technical note ; NASA TN D-6917
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Snyder, Roger W. q| (Roger William)
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    a| Analytical study of effect of casing treatment on performance of a multistage compressor c| by Roger W. Snyder and Robert J. Blade.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1972.
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    a| 24 p. : b| ill. ; c| 27 cm.
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    a| NASA technical note ; v| NASA TN D-6917
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    a| Prepared at Lewis Research Center.
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    a| Cover title.
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    a| Bibliography: p. 14.
    520
      
      
    a| The simulation was based on individual stage pressure and efficiency maps. These maps were modified to account for casing treatment effects on the individual stage characteristics. The individual stage maps effects on overall compressor performance were observed. The results show that to improve the performance of the compressor in its normal operating range, casing treatment of the rear stages is required.
    538
      
      
    a| Mode of access: Internet.
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    0
    0
    a| Simulation.
    650
      
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    a| Axial flow compressors x| Mathematical models.
    700
    1
      
    a| Blade, Robert J.
    710
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    a| United States. b| National Aeronautics and Space Administration.
    710
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    a| Lewis Research Center.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106886200 y| 1972 r| pd q| bib

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