Item Details

Aerodynamic Damping at Mach Numbers of 1.3 and 1.6 of a Control Surface on a Two-Dimensional Wing by the Free-Oscillation Method

by W.J. Tuovila and Robert W. Hess
Format
Book; Government Document; Online; EBook
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Language
English
Series
NASA Technical Note
Description
21 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "NASA TN D-116."
  • "Langley Research Center, Langley Field, Va."
  • "February 1960."
  • Title from cover.
  • Includes bibliographical references (p. 11).
Series Statement
NASA technical note ; D-116
Other Forms
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/11/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068196_1989068196.pdf.
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method / c| by W.J. Tuovila and Robert W. Hess.
    260
      
      
    a| Washington, [D.C.] : b| National Aeronautics and Space Administration, c| 1960.
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    a| 21 p. : b| ill. ; c| 26 cm.
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    a| NASA technical note ; v| D-116
    500
      
      
    a| "NASA TN D-116."
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    a| "Langley Research Center, Langley Field, Va."
    500
      
      
    a| "February 1960."
    500
      
      
    a| Title from cover.
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    a| Includes bibliographical references (p. 11).
    530
      
      
    a| Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/11/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068196_1989068196.pdf.
    538
      
      
    a| Mode of access: Internet.
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    7
    a| Steels. 2| nasat
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    7
    a| Magnesium. 2| nasat
    650
      
    7
    a| Mach number. 2| nasat
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    7
    a| Aluminum. 2| nasat
    650
      
    7
    a| Aircraft stability. 2| nasat
    650
      
    7
    a| Wing profiles. 2| nasat
    650
      
    7
    a| Vibration damping. 2| nasat
    650
      
    7
    a| Supersonic flutter. 2| nasat
    650
      
    7
    a| Supersonic airfoils. 2| nasat
    650
      
    7
    a| Free vibration. 2| nasat
    650
      
    7
    a| Control surfaces. 2| nasat
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    a| Hess, R. W. q| (Robert W.)
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    a| Langley Research Center.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106742544 y| 1960 r| pd q| bib

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