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Cooled-Turbine Aerodynamic Performance Prediction From Reduced Primary to Coolant Total-Temperature-Ratio Results

Louis J. Goldman ; Lewis Research Center, Cleveland, Ohio
Format
Book; Government Document
Published
Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976.
Language
English
Series
NASA Technical Note
Description
[1], 41 p. : ill. ; 27 cm.
Notes
  • Cover title.
  • Bibliography: p. 34-35.
Series Statement
NASA technical note NASA TN D-8312
Technical Details
  • Access in Virgo Classic
  • Staff View

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    c| $4.00
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    a| Cooled-turbine aerodynamic performance prediction from reduced primary to coolant total-temperature-ratio results / c| Louis J. Goldman ; Lewis Research Center, Cleveland, Ohio.
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    a| Washington : b| U.S. National Aeronautics and Space Administration ; a| Springfield, Va. : b| for sale by the National Technical Information Service, c| 1976.
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    a| [1], 41 p. : b| ill. ; c| 27 cm.
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    0
    a| NASA technical note v| NASA TN D-8312.
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    a| Cover title.
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    a| Bibliography: p. 34-35.
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    0
    a| Turbines x| Aerodynamics.
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    a| Lewis Research Center.
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    a| Readex MicPrnt 77-786 w| SUDOC i| 1392851-1001 l| BY-REQUEST m| IVY t| BOOK
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