Item Details

Turbulent Heat-Transfer Prediction Method for Application to Scramjet Engines

by S.Z. Pinckney
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], 1974.
Language
English
Series
NASA Technical Note
Description
64 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
  • Includes bibliographical references (p. 33-35).
Series Statement
NASA technical note ; NASA TN D-7810
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| TL521 b| .A3525 no. 7810
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    a| Pinckney, S. Z. q| (Shimer Zane), d| 1934-
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    a| Turbulent heat-transfer prediction method for application to scramjet engines / c| by S.Z. Pinckney.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1974.
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    a| 64 p. : b| ill. ; c| 27 cm.
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    0
      
    a| NASA technical note ; v| NASA TN D-7810
    500
      
      
    a| Prepared at Langley Research Center.
    500
      
      
    a| Cover title.
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    a| Includes bibliographical references (p. 33-35).
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    a| Mode of access: Internet.
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    a| Combustion chambers x| Cooling.
    650
      
    0
    a| Turbulent boundary layer.
    650
      
    0
    a| Heat x| Transmission.
    650
      
    0
    a| Airplanes x| Ramjet engines x| Cooling.
    710
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    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106915264 y| 1974 r| pd q| bib

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