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Analytical Methodology for Predicting the Onset of Widespread Fatigue Damage in Fuselage Structure [microform]

C.E. Harris ... [et al.]
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:110293
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 110293
Technical Details
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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| 1996]
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    a| Fuselages. 2| nasat
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    7
    a| Residual strength. 2| nasat
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    7
    a| Crack initiation. 2| nasat
    650
      
    7
    a| Crack propagation. 2| nasat
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    a| Fatigue (Materials) 2| nasat
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    7
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Alderman 3rd Floor East Reading Room N/A Available Non-Circ.