Item Details

Investigation of the Effect of a Guide-Vane-Rotor Combination on Inlet Total-Pressure Distortions in a Compressible Fluid

by George C. Ashby, Jr.
Format
Book; Government Document; Online; EBook
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Language
English
Series
NASA Technical Note
Description
15 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "NASA TN D-123."
  • "Langley Research Center, Langley Field, Va."
  • "December 1959."
  • Title from cover.
  • Includes bibliographical references (p. 11).
Series Statement
NASA technical note ; D-123
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/19890068383_1989068383.pdf.
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid / c| by George C. Ashby, Jr.
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    a| Washington, [D.C.] : b| National Aeronautics and Space Administration, c| 1959.
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    a| 15 p. : b| ill. ; c| 26 cm.
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    a| NASA technical note ; v| D-123
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    a| "NASA TN D-123."
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    a| "Langley Research Center, Langley Field, Va."
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    a| "December 1959."
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    a| Title from cover.
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    a| Includes bibliographical references (p. 11).
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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/19890068383_1989068383.pdf.
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    a| Mode of access: Internet.
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    a| Jet aircraft. 2| nasat
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    a| Density (mass volume) 2| nasat
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    a| Compressors. 2| nasat
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    a| Rotors. 2| nasat
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    a| Pressure distribution. 2| nasat
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    a| Inlet pressure. 2| nasat
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    7
    a| Inlet flow. 2| nasat
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    a| Guide vanes. 2| nasat
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    a| Flow distortion. 2| nasat
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