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Effect of Angular Inflow on the Vibratory Response of a Counter-Rotating Propeller [microform]: By J.E. Turnberg, P.C. Brown

Turnberg, J. E; Brown, P C; United States National Aeronautics and Space Administration
Format
Book; Government Document; Microform
Published
[Washington, DC] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:174819
Description
1 v.
Notes
Distributed to depository libraries in microfiche.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 1 microfiche.
Series Statement
NASA contractor report NASA CR-174819
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| N 87-10840 b| NASA
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    a| GPO c| GPO d| DLC d| MvI
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    a| Effect of angular inflow on the vibratory response of a counter-rotating propeller h| [microform] : b| by J.E. Turnberg, P.C. Brown.
    260
      
      
    a| [Washington, DC] : b| NASA ; a| [Springfield, Va. : b| For sale by the National Technical Information Service, c| 1985]
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    a| 1 v.
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    0
    a| NASA contractor report v| NASA CR-174819
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    a| Distributed to depository libraries in microfiche.
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    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1986] e| 1 microfiche.
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    a| 2
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    7
    a| Counter rotation. 2| nasat
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    7
    a| Propeller blades. 2| nasat
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    a| Vibratory loads. 2| nasat
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    a| Brown, P. C.
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    a| United States. b| National Aeronautics and Space Administration.
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    a| NAS 1.26:174819 w| SUDOC i| 2502594-1001 l| 3EAST m| ALDERMAN t| MICROFICHE
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Alderman 3rd Floor East Reading Room N/A Available Non-Circ.