Item Details

The Effects of an Inverse-Taper Leading-Edge Flap on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing at Mach Numbers to 0.90

by Fred A. Demele
Format
Book; Government Document; Online; EBook
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Language
English
Series
NASA Technical Note
Description
108 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "NASA TN D-138."
  • "Ames Research Center, Moffett Field, Calif."
  • "December 1959."
  • Title from cover.
  • Includes bibliographical references (p. 7).
Series Statement
NASA technical note ; D-138
Other Forms
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/12/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068200_1989068200.pdf.
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Technical Details

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    a| The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 / c| by Fred A. Demele.
    260
      
      
    a| Washington, [D.C.] : b| National Aeronautics and Space Administration, c| 1959.
    300
      
      
    a| 108 p. : b| ill. ; c| 26 cm.
    490
      
    0
    a| NASA technical note ; v| D-138
    500
      
      
    a| "NASA TN D-138."
    500
      
      
    a| "Ames Research Center, Moffett Field, Calif."
    500
      
      
    a| "December 1959."
    500
      
      
    a| Title from cover.
    504
      
      
    a| Includes bibliographical references (p. 7).
    530
      
      
    a| Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/12/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068200_1989068200.pdf.
    538
      
      
    a| Mode of access: Internet.
    650
      
    7
    a| Wind tunnel tests. 2| nasat
    650
      
    7
    a| Twisting. 2| nasat
    650
      
    7
    a| Pressure effects. 2| nasat
    650
      
    7
    a| Mach number. 2| nasat
    650
      
    7
    a| Deflection. 2| nasat
    650
      
    7
    a| Camber. 2| nasat
    650
      
    7
    a| Aspect ratio. 2| nasat
    650
      
    7
    a| Wing profiles. 2| nasat
    650
      
    7
    a| Wing loading. 2| nasat
    650
      
    7
    a| Sweptback wings. 2| nasat
    650
      
    7
    a| Leading edge flaps. 2| nasat
    650
      
    7
    a| Aerodynamic loads. 2| nasat
    710
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    a| Ames Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106742064 y| 1959 r| pd q| bib

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