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Amplified Crossflow Disturbances in the Laminar Boundary Layer on Swept Wings With Suction

J. Ray Dagenhart
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1902
Description
87 p. : ill. ; 28 cm.
Notes
  • "Langley Research Center."
  • "November 1981"--Cover.
  • Subject Category 34.
  • Includes bibliographical references.
Series Statement
NASA technical paper 1902
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction / c| J. Ray Dagenhart.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Branch ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1981.
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    a| NASA technical paper v| 1902
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    a| "Langley Research Center."
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    a| Subject Category 34.
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    a| Includes bibliographical references.
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    a| Airplanes x| Wings, Swept-back x| Mathematical models.
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    a| Laminar flow x| Mathematical models.
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    0
    a| Boundary layer x| Mathematical models.
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    a| United States. b| National Aeronautics and Space Administration. b| Scientific and Technical Information Branch.
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