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Performance and Vibratory Loads Data From a Wind-Tunnel Test of a Model Helicopter Main-Rotor Blade With a Paddle-Type Tip [microform]

William T. Yeager, Jr. ... [et al.]
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : National Technical Information Service, distribution, 1997]
Language
English
Series
NASA Technical Memorandum
ARL Technical Report
ATCOM Technical Report
SuDoc Number
NAS 1.15:4754
Description
1 v.
Notes
Shipping list no.: 98-0613-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and space Administration, 1997] 1 microfiche.
Series Statement
NASA technical memorandum 4754
ARL technical report ; 1283
ATCOM technical report ; 97-A-006
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip h| [microform] / c| William T. Yeager, Jr. ... [et al.].
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    a| Hampton, Va. : b| National Aeronautics and Space Administration, Langley Research Center ; a| [Springfield, VA : b| National Technical Information Service, distribution, c| 1997]
    300
      
      
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    440
      
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    a| NASA technical memorandum v| 4754
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    0
      
    a| ARL technical report ; v| 1283
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    a| ATCOM technical report ; v| 97-A-006
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    a| Rotary wings. 2| nasat
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    7
    a| Performance tests. 2| nasat
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    7
    a| Vibratory loads. 2| nasat
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    a| Wind tunnel tests. 2| nasat
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    a| Paddles. 2| nasat
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