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Experimental Verification of a Progressive Damage Model for IM7/5260 Laminates Subjected to Tension-Tension Fatigue [microform]

Timothy W. Coats, Charles E. Harris
Format
Book; Government Document; Microform
Published
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Language
English
Series
NASA-TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:111921
Description
1 v.
Notes
Shipping list no.: 98-0599-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Series Statement
NASA-TM ; 111921
NASA technical memorandum 111921
Technical Details
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  • Staff View

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    a| Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue h| [microform] / c| Timothy W. Coats, Charles E. Harris.
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    a| Aircraft structures. 2| nasat
    650
      
    7
    a| Finite element method. 2| nasat
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    7
    a| Resin matrix composites. 2| nasat
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    7
    a| Crack propagation. 2| nasat
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    7
    a| Stiffness. 2| nasat
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    a| Delaminating. 2| nasat
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