Item Details

Sweep Effect on the Drag of Rows of Perpendicular Circular Cylinders in a Laminar Boundary Layer at Supersonic Free-Stream Velocities

by Milton Lamb and Robert L. Stallings, Jr.
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
16 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
  • Includes bibliographical references (p. 8).
Series Statement
NASA technical note ; NASA TN D-7812
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / c| by Milton Lamb and Robert L. Stallings, Jr.
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    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| 16 p. : b| ill. ; c| 27 cm.
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    a| NASA technical note ; v| NASA TN D-7812
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    a| Prepared at Langley Research Center.
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    a| Cover title.
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    a| Includes bibliographical references (p. 8).
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    a| Mode of access: Internet.
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    a| Aerodynamics, Supersonic.
    650
      
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    a| Boundary layer.
    650
      
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    a| Laminar flow.
    650
      
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    a| Cylinders.
    650
      
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    a| Drag (Aerodynamics)
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    a| Stallings, Robert L.
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    a| Langley Research Center.
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