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Computational Test Cases for a Rectangular Supercritical Wing Undergoing Pitching Oscillations [microform]

Robert M. Bennett and Charlotte E. Walker
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:209130
Description
1 v.
Notes
Shipping list no.: 1999-0729-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 2 microfiches.
Series Statement
[NASA technical memorandum] ; NASA/TM-1999-209130
NASA technical memorandum 209130
Technical Details
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  • Staff View

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    a| NAS 1.15:209130
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    a| Computational test cases for a rectangular supercritical wing undergoing pitching oscillations h| [microform] / c| Robert M. Bennett and Charlotte E. Walker.
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    a| Hampton, Va. : b| National Aeronautics and Space Administration, Langley Research Center ; a| Springfield, VA : b| National Technical Information Service, distributor, c| [1999]
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    a| Shipping list no.: 1999-0729-M.
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    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1999] e| 2 microfiches.
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    7
    a| Computational fluid dynamics. 2| nasat
    650
      
    7
    a| Unsteady aerodynamics. 2| nasat
    650
      
    7
    a| Rectangular wings. 2| nasat
    650
      
    7
    a| Supercritical wings. 2| nasat
    650
      
    7
    a| Wing oscillations. 2| nasat
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    7
    a| Wind tunnel tests. 2| nasat
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    a| Walker, Charlotte E.
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    a| NASA technical memorandum v| 209130.
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