Item Details

Rotary Balance Data for a Typical Single-Engine General Aviation Design for an Angle-of-Attack Range of 8 ̊to 35.̊: III Effect of Wing Leading-Edge Modifications Model a

William Bihrle, Jr., and William Mulcay
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1979.
Language
English
Series
NASA Contractor Report
Description
18, A1-A155 p. : chiefly ill. ; 27 cm.
Mode of access: Internet.
Notes
  • "November 1979"--Cover.
  • "Prepared [at Bihrle Applied Research] for Langley Research Center under contract NAS1-14849."
  • Includes bibliographical references (p. 8).
Series Statement
NASA contractor report ; 3102
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| TL521.3.C6 b| A3 no. 3102
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    a| Bihrle, William.
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    a| Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 35.̊ n| III, p| Effect of wing leading-edge modifications model A / c| William Bihrle, Jr., and William Mulcay.
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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| 1979.
    300
      
      
    a| 18, A1-A155 p. : b| chiefly ill. ; c| 27 cm.
    490
    0
      
    a| NASA contractor report ; v| 3102
    500
      
      
    a| "November 1979"--Cover.
    500
      
      
    a| "Prepared [at Bihrle Applied Research] for Langley Research Center under contract NAS1-14849."
    504
      
      
    a| Includes bibliographical references (p. 8).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Wind tunnel balances.
    650
      
    0
    a| Spin (Aerodynamics)
    650
      
    0
    a| Private planes.
    650
      
    0
    a| Leading edges (Aerodynamics)
    650
      
    0
    a| Aerodynamic measurements.
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    a| Mulcay, William.
    710
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    a| Langley Research Center.
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    a| Bihrle Applied Research, Inc.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106737643 y| 1979 r| pd q| bib

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