HEA|  |01449nam  2200253Ia 4500
001|  |021997014227
003|  |OCoLC
005|  |20050607095353.0
008|  |001020m19731975ohu      t   f000 0 eng d
040|  |▼aCAI▼cCAI▼dOCLCQ▼dCIN
093|  |▼aV215.6▼23
245|00|▼aDevelopment and evaluation o-
   |  |f methods of plane stress frac-
   |  |ture analysis.
260|  |▼aDayton, Ohio :▼bAir Force Fl-
   |  |ight Dynamics Laboratory,▼c1973-1975.
300|  |▼a3 v. \'▼c26 cm.
500|  |▼aFinal report.
505|0 |▼a[pt. 1] Review / R.M. Verett-
   |  |e －－ pt. 2, v. 1. A technique -
   |  |for predicting residual streng-
   |  |th of structure / M.M. Ratwani-
   |  |, D.P. Wilhelm －－ pt. 2, v. 2.-
   |  | Fracture resistance and mater-
   |  |ial property characterization -
   |  |/ D.P. Wilhem, J.H. Fitzgerald-
   |  | －－ pt. 3. Application of the -
   |  |residual strength prediction t-
   |  |echnique to complex aircraft s-
   |  |tructure / M.M. Ratwani and D.P. Wilhem.
700|1 |▼aVerette, R. M.
700|12|▼aRatwani, M. M.▼tTechnique fo-
   |  |r predicting residual strength-
   |  | of structure.
700|12|▼aWilhem, D. P.▼tFracture resi-
   |  |stance and material property c-
   |  |haracterization.
700|12|▼aRatwani, M. M.▼tApplication -
   |  |of the residual strength predi-
   |  |ction technique to complex air-
   |  |craft structure.
710|2 |▼aNorthrop Corporation.▼bAircr-
   |  |aft Division.
830| 0|▼aTechnical report (Air Force -
   |  |Flight Dynamics Laboratory (U.-
   |  |S.)) ;▼vAFFDL-TR-73-42.
950|  |▼aJ▼fV215.6/D489
999|  |▼tC▼Atshs11▼a20050607 09:49:28-
   |  |▼Mtshs11▼m20050607 09:53:53▼Gt-
   |  |shs11▼g20050607 09:54:40

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