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Influence of Coolant Tube Curvature on Film Cooling Effectiveness as Detected by Infrared Imagery

S. Stephen Papell, Robert W. Graham, and Richard P. Cageao
Format
EBook; Book; Government Document; Online
Published
Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1979.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1546
Description
1 online resource (14 pages) : illustrations.
Notes
  • Title from title screen (viewed Sept. 22, 2014).
  • "November 1979."
  • "Performing organization, Lewis Research Center"--Technical report documentation page.
  • Includes bibliographical references (page 8).
Series Statement
NASA technical paper ; 1546
NASA technical paper 1546
Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| text b| txt 2| rdacontent
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    a| "November 1979."
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    a| "Performing organization, Lewis Research Center"--Technical report documentation page.
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    a| Includes bibliographical references (page 8).
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    a| Sponsored by National Aeronautics and Space Administration h| 505-04
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    0
    a| Cooling curves.
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    0
    a| Infrared detectors.
    650
      
    0
    a| Vortex tubes.
    650
      
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    a| Coolants. 2| nasat
    650
      
    7
    a| Cooling. 2| nasat
    650
      
    7
    a| Film cooling. 2| nasat
    650
      
    7
    a| Hilsch tubes. 2| nasat
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    7
    a| Infrared imagery. 2| nasat
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    7
    a| Heat transfer. 2| nasat
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    i| Print version: a| Papell, S. Stephen. t| Influence of coolant tube curvature on film cooling effectiveness as detected by infrared imagery w| (OCoLC)8086988
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    a| Graham, Robert W., e| author.
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    a| Cageao, Richard P. e| author.
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    a| United States. b| National Aeronautics and Space Administration. b| Scientific and Technical Information Branch e| issuing body.
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    a| NAS 1.60:1546 w| SUDOC i| 6425998-1001 l| INTERNET m| UVA-LIB t| INTERNET
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