Item Details

Aerodynamic Characteristics of Several Current Helicopter Tail Boom Cross Sections Including the Effect of Spoilers

John C. Wilson and Henry L. Kelley
Format
Book; Government Document; Online; EBook
Published
[Washington, DC] : National Aeronautics and Space Administration, 1986.
Language
English
Series
Usaavscom Tr
NASA Tp
Access Restriction
Approved for public release; distribution unlimited.
Description
72 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • STAR Subject category 02.
  • "January 1986."
  • References: p. 6. 8
Series Statement
USAAVSCOM TR ; 85-B-3
NASA TP ; 2506
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers / c| John C. Wilson and Henry L. Kelley.
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    a| [Washington, DC] : b| National Aeronautics and Space Administration, c| 1986.
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    a| 72 p. : b| ill. ; c| 28 cm.
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    a| USAAVSCOM TR ; v| 85-B-3
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    a| NASA TP ; v| 2506
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    a| STAR Subject category 02.
    500
      
      
    a| "January 1986."
    504
      
      
    a| References: p. 6. b| 8
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    a| Approved for public release; distribution unlimited.
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    a| Technical report.
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    a| Mode of access: Internet.
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    7
    a| Spoilers. 2| ddcrit
    650
      
    7
    a| Tail helicopter rotors. 2| ddcrit
    650
      
    7
    a| Tails (Aircraft) 2| ddcrit
    650
      
    7
    a| Aeronautical booms. 2| ddcrit
    650
      
    7
    a| Wind tunnel tests. 2| ddcrit
    650
      
    7
    a| Aerodynamics. 2| ddcrit
    650
      
    7
    a| Helicopters x| Tails. 2| ddcrit
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    1
      
    a| Kelley, Henry L. 4| org. u| AVSCOM.
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    a| United States. b| Army Aviation Research and Technology Activity. b| Aerostructures Directorate.
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    a| Langley Research Center.
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    1
      
    a| United States. b| Army Aviation Systems Command.
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    1
      
    a| United States. b| National Aeronautics and Space Administration.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106614446 y| 1986 r| pd

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