LEADER 02274cam a2200481Ka 4500001    9951566563506421
005    20221219145548.0
008    980722s1992    vaua    bb   f000 0 eng d
035    (NjP)5156656-princetondb
035    (OCoLC)ocm39527508
035     |z(NjP)Voyager5156656
040    GPO |beng |cGPO |dGPO |dMvI
049    DOCS
074    0830-D (MF)
074    0830-D (online)
086 0  NAS 1.15:104159/REV. |zNAS 1.15:104159
100 1  Newman, J. C. |0http://id.loc.gov/authorities/names/n82227083
245 10 FASTRAN-II |h[microform] : |ba fatigue crack growth structural analysis program / |cJ.C. Newman, Jr.
246 30 Fatigue crack growth structural analysis program
250    Feb. 1992 (rev. copy).
260    Hampton, Va. : |bNational Aeronautics and Space Administration, Langley Research Center ;Springfield, Va. : |bNational Technical Information Service, distributor], |c1992.
300    1 v.
440  0 NASA technical memorandum ; |v104159
500    Shipping list no.: 1993-0009-M.
504    Includes bibliographical references.
533    Microfiche. |b[Washington, D.C. : |cNational Aeronautics and Space Administration, |d1993]. |e2 microfiches.
530    Also available via Internet from the NTRS web site. Address as of 3/6/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920021720%5F1992021720.pdf; current access is available via PURL.
650  7 Crack closure. |2nasat
650  7 Crack properties. |2nasat
650  7 Crack tips. |2nasat
650  7 Cracks. |2nasat
650  7 Cyclic loads. |2nasat
650  7 Fatigue (materials) |2nasat
650  7 Plastic deformation. |2nasat
650  7 Stress concentration. |2nasat |0http://id.loc.gov/authorities/subjects/sh85128706
650  7 Stress intensity factors. |2nasat
650  7 Structural analysis. |2nasat
650  7 Structural design. |2nasat |0http://id.loc.gov/authorities/subjects/sh85129194
650  7 User manuals (computer programs) |2nasat
710 2  Langley Research Center. |0http://id.loc.gov/authorities/names/n79134855
945    DOCS |cNAS 1.15:104159/REV.