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| 035 | ⊔ | ⊔ | ‡a(MiU)99187539638706381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187539638706381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)429484244 |
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| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡cLHL ‡dOCLCO ‡dOCLCQ ‡dOCLCF ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/57:79:3095/Volume III |
| 088 | ⊔ | ⊔ | ‡aADA 115185 |
| 088 | ⊔ | ⊔ | ‡aAFWAL TR 79-3095/V.3 |
| 100 | 1 | ⊔ | ‡aLauraitis, K. N., ‡eauthor. |
| 245 | 1 | 0 | ‡aAdvanced residual strength degradation rate modeling for advanced composite structures. ‡nVolume 3. ‡pAppendixes to report for Tasks II and III / ‡cK.N. Lauraitis, J.T. Ryder, D.E. Pettit. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bFlight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, ‡c1981. |
| 300 | ⊔ | ⊔ | ‡axliv, 379 pages : ‡billustrations, figures, tables ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAFWAL-TR (Air Force Wright Aeronautical Laboratories) ; ‡vAFWAL-TR-79-3095/Volume III |
| 500 | ⊔ | ⊔ | ‡a"The program was conducted by the Structures and Materials Department of the Lockheed-California Company." |
| 500 | ⊔ | ⊔ | ‡a"Final Report for 1 July 1979 to 29 May 1981." |
| 500 | ⊔ | ⊔ | ‡aADA115185 (from http://www.dtic.mil). |
| 500 | ⊔ | ⊔ | ‡a"Contains appendices." |
| 500 | ⊔ | ⊔ | ‡a"July 1981." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 520 | ⊔ | ⊔ | ‡aThis report presents the results of the first task of the last two tasks of a three-task program focusing on the study of relationship between damage propagation and residual strength of graphite/epoxy laminates. Specimens of two laminate types, a 32-ply quasi-isotropic and 24-ply 67%-0, containing a centered poorly drilled hole were evaluated in this study. Baseline static tension and compression tests were conducted at high and low strain rates and at elevated temperature. |
| 536 | ⊔ | ⊔ | ‡aAir Force Contract No. ‡bF33615-77-C-3084, Project 2401, Work Unit 24010117. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aNondestructive testing. |
| 650 | ⊔ | 0 | ‡aStrength of materials. |
| 650 | ⊔ | 0 | ‡aGraphite. |
| 650 | ⊔ | 0 | ‡aMaterials ‡xFatigue. |
| 650 | ⊔ | 0 | ‡aLaminated materials. |
| 650 | ⊔ | 0 | ‡aComposite materials. |
| 700 | 1 | ⊔ | ‡aPettit, D. E., ‡eauthor. |
| 700 | 1 | ⊔ | ‡aRyder, J. T., ‡eauthor. |
| 710 | 2 | ⊔ | ‡aAir Force Wright Aeronautical Laboratories, ‡eissuing agency. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 710 | 2 | ⊔ | ‡aLockheed-California Company, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 776 | 0 | 8 | ‡iOnline version: ‡aLauraitis, K. N. ‡tAdvanced Residual Strength Degradation Rate Modeling for Advanced Composite Structures. ‡dWright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981 ‡w(OCoLC)1103216031 |
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| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20240607 ‡sgoogle ‡umdp.39015095334622 ‡y1981 ‡rpd ‡qbib ‡tUS fed doc |