Item Details

Method for Predicting Off-Design Performance of Axial-Flow Compressor Blade Rows

by George K. Serovy and E.W. Anderson
Format
Book; Government Document; Online; EBook
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Language
English
Series
NASA Technical Note
Description
37 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "NASA TN D-110."
  • "Iowa State College."
  • "August 1959."
  • Title from cover.
  • Includes bibliographical references (p. 22-24).
Series Statement
NASA technical note ; D-110
Other Forms
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/11/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068302_1989068302.pdf.
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Technical Details

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    a| Method for predicting off-design performance of axial-flow compressor blade rows / c| by George K. Serovy and E.W. Anderson.
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    a| Washington, [D.C.] : b| National Aeronautics and Space Administration, c| 1959.
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    a| 37 p. : b| ill. ; c| 26 cm.
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    a| NASA technical note ; v| D-110
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    a| "NASA TN D-110."
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    a| "Iowa State College."
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    a| "August 1959."
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    a| Title from cover.
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    a| Includes bibliographical references (p. 22-24).
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    a| Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/11/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068302_1989068302.pdf.
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    a| Mode of access: Internet.
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    7
    a| Rotor speed. 2| nasat
    650
      
    7
    a| Pressure ratio. 2| nasat
    650
      
    7
    a| Mach number. 2| nasat
    650
      
    7
    a| Guide vanes. 2| nasat
    650
      
    7
    a| Flow velocity. 2| nasat
    650
      
    7
    a| Flow equations. 2| nasat
    650
      
    7
    a| Cascade flow. 2| nasat
    650
      
    7
    a| Turbocompressors. 2| nasat
    650
      
    7
    a| Performance prediction. 2| nasat
    650
      
    7
    a| Compressor efficiency. 2| nasat
    650
      
    7
    a| Compressor blades. 2| nasat
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    7
    a| Axial flow. 2| nasat
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