Item Details

Mass Transfer Cooling Near the Stagnation Point

by Leonard Roberts
Format
Book; Government Document; Online; EBook
Published
Washington, DC : U.S. G.P.O., 1959.
Language
English
Series
NASA Tr
Abstract
A simplified analysis is made of mass transfer cooling--that is, injection of a foreign gas--near the stagnation point for two-dimensional and axisymmetric bodies. The reduction in heat transfer is given in terms of the properties of the coolant gas and it is shown that the heat transfer may be reduced considerably by the introduction of a gas having appropriate thermal and diffusive properties. The mechanism by which heat transfer is reduced is discussed.
Description
16 p. ; 26 cm.
Mode of access: Internet.
Notes
  • "Report date July 3, 1958."
  • Includes bibliographical references (p. 16).
Series Statement
NASA TR ; R-8
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Mass transfer cooling near the stagnation point / c| by Leonard Roberts.
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    a| Washington, DC : b| U.S. G.P.O., c| 1959.
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    a| 16 p. ; c| 26 cm.
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    a| NASA TR ; v| R-8
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    a| "Report date July 3, 1958."
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    a| Includes bibliographical references (p. 16).
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    3
      
    a| A simplified analysis is made of mass transfer cooling--that is, injection of a foreign gas--near the stagnation point for two-dimensional and axisymmetric bodies. The reduction in heat transfer is given in terms of the properties of the coolant gas and it is shown that the heat transfer may be reduced considerably by the introduction of a gas having appropriate thermal and diffusive properties. The mechanism by which heat transfer is reduced is discussed.
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Laminar flow.
    650
      
    0
    a| Heat x| Transmission.
    710
    1
      
    a| United States. b| National Aeronautics and Space Administration.
    710
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    a| Langley Research Center.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106908483 y| 1959 r| pd q| bib

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