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| 035 | ⊔ | ⊔ | ‡a(MiU)99187539589006381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187539589006381 |
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| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡cLHL ‡dOCLCO ‡dOCLCQ ‡dOCLCF ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/26-2:61-667/V.1 |
| 088 | ⊔ | ⊔ | ‡aAD 277029 |
| 088 | ⊔ | ⊔ | ‡aASD TR 61-667/V.1 |
| 100 | 1 | ⊔ | ‡aHuang, P. C., ‡eauthor. |
| 245 | 1 | 0 | ‡aElasto-plastic analysis of structures under load and two-dimensional temperature distributions. ‡nVolume 1, ‡pAnalysis development and experimental program / ‡cP.C. Huang and R.J. Edwards. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bFlight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, ‡c1962. |
| 300 | ⊔ | ⊔ | ‡aviii, 108 pages : ‡billustrations ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aASD technical report ; ‡v61-667/V.1 |
| 500 | ⊔ | ⊔ | ‡aAD0277029 (from http://www.dtic.mil). |
| 500 | ⊔ | ⊔ | ‡a"April 1962." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (page 36). |
| 520 | ⊔ | ⊔ | ‡aThis report describes investigations performed to determine experimentally the validity of the time-independent aspects of a time-dependent elasto-plastic stress and strain analysis method for structures exposed to complex load and two-dimensional elevated temperature environments. Experiments, consisting of tests of long flat plates subjected to uniaxial loads and temperatures which varied in two directions, are described. These were specificially designed to evaluate the accuracy of the analysis method. Magnitude and duration of the test variables were such that the strains induced by loading were in the plastic range and appreciable thermal stress systems were induced. Significant creep strains were eliminated by short-time continuous loading. Experimental strains were compared with analytical strains calculated for conditions indentical with the tests. Within the range of test parameters selected, the degree of correlation achieved indicates verification of the time-independent portion of the analysis method. |
| 536 | ⊔ | ⊔ | ‡aResearch supported by the United States Air Force, Air Force Systems Command, and performed by Martin-Marietta Corporation, Baltimore Division, under Contract No. ‡bAF 33(616)-7738. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aStrains and stresses. ‡2fast ‡0(OCoLC)fst01134288 |
| 650 | ⊔ | 7 | ‡aPlasticity. ‡2fast ‡0(OCoLC)fst01066531 |
| 650 | ⊔ | 7 | ‡aElasticity. ‡2fast ‡0(OCoLC)fst00904211 |
| 650 | ⊔ | 7 | ‡aAirframes. ‡2fast ‡0(OCoLC)fst00802910 |
| 650 | ⊔ | 7 | ‡aAerodynamic heating. ‡2fast ‡0(OCoLC)fst00798175 |
| 650 | ⊔ | 0 | ‡aStrains and stresses. |
| 650 | ⊔ | 0 | ‡aAerodynamic heating. |
| 650 | ⊔ | 0 | ‡aPlasticity. |
| 650 | ⊔ | 0 | ‡aElasticity. |
| 650 | ⊔ | 0 | ‡aDeformations (Mechanics) |
| 650 | ⊔ | 0 | ‡aAirframes. |
| 700 | 1 | ⊔ | ‡aEdwards, R. J., ‡eauthor. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bAir Force. ‡bSystems Command. ‡bAeronautical Systems Division, ‡eissuing body. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.) ‡esponsor. |
| 710 | 2 | ⊔ | ‡aMartin Marietta Corporation. ‡bBaltimore Division, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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