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Application of Interface Technology in Nonlinear Analysis of a Stitched/RFI Composite Wing Stub Box [microform]

John T. Wang and Jonathan B. Ransom
Format
EBook; Book; Government Document; Microform; Online
Published
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:112837
Description
1 v.
Notes
Shipping list no.: 1998-0613-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche. (NASA-TM ; 112837).
Series Statement
NASA technical memorandum 112837
Other Forms
Also available via Internet from the NASA Web site. Address as of 12/27/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.g ov/19970019491%5F1997029263.pdf; current access available via PURL.
Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
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    003 SIRSI
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    a| (Sirsi) tmp97212188
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    037
      
      
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    1
      
    a| Wang, John T.
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    0
    a| Application of interface technology in nonlinear analysis of a stitched/RFI composite wing stub box h| [microform] / c| John T. Wang and Jonathan B. Ransom.
    260
      
      
    a| [Washington, D.C. : b| National Aeronautics and Space Administration ; a| Springfield, Va. : b| National Technical Information Service, distributor, c| 1997]
    300
      
      
    a| 1 v.
    500
      
      
    a| Shipping list no.: 1998-0613-M.
    530
      
      
    a| Also available via Internet from the NASA Web site. Address as of 12/27/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.g ov/19970019491%5F1997029263.pdf; current access available via PURL.
    533
      
      
    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1997] e| 1 microfiche. f| (NASA-TM ; 112837).
    596
      
      
    a| 2
    650
      
    7
    a| Wings. 2| nasat
    650
      
    7
    a| Composite structures. 2| nasat
    650
      
    7
    a| Bending. 2| nasat
    650
      
    7
    a| Finite element method. 2| nasat
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    a| Aircraft structures. 2| nasat
    650
      
    7
    a| Structural analysis. 2| nasat
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    a| Ransom, Jonathan B.
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    a| NASA technical memorandum v| 112837.
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