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| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:68-56/Volume I |
| 088 | ⊔ | ⊔ | ‡aAD 0685190 |
| 088 | ⊔ | ⊔ | ‡aAFFDL TR 68-56/V.1 |
| 100 | 1 | ⊔ | ‡aMallett, Robert H., ‡eauthor. |
| 245 | 1 | 0 | ‡aMAGIC : ‡bn automated general purpose system for structural analysis. ‡nVolume 1, ‡pEngineer's manual / ‡cRobert H. Mallett, Stephen Jordon. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, ‡c1969. |
| 300 | ⊔ | ⊔ | ‡axiii, 214 pages : ‡billustrations, figures ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 68-56/Volume I |
| 500 | ⊔ | ⊔ | ‡a"This report was prepared by Textron's Bell Aerosystems, Buffalo, New York, under USAF Contract No. AF 33 (615)-57-C-1505, Project No. 1467, Task No. 146702." |
| 500 | ⊔ | ⊔ | ‡a"Bell Aerosystems, a Textron Company." |
| 500 | ⊔ | ⊔ | ‡a"January 1969." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (pages 211-214). |
| 520 | ⊔ | ⊔ | ‡aAn automated general purpose system for analysis is presented. This system, identified by the aconym 'MAGIC' for 'Matrix Analysis via Generative and Interpretive Computations, ' provides a flexible framework for implementation of the finite element analysis technology. Powerful capabilities for displacement, stress and stability analyses are included in the subject MAGIC System for structural analysis. The matrix displacement method of analysis based upon finite element idealization is employed throughout. Six versatile finite elements are incorporated in the finite element library. These are: frame, shear panel, triangular cross-section ring, toroidal thin shell ring, quadrilateral thin shell and triangular thin shell elements. These finite element representations include matrices for stiffness, incremental stiffness, perstrain load, thermal load, distributed mechanical load and stress. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 583 | 1 | ⊔ | ‡awill digitize ‡c20200915 ‡zQueued for digitization ‡cSeptember 15, 2020 ‡5miu ‡2pda |
| 650 | ⊔ | 0 | ‡aStability. |
| 650 | ⊔ | 0 | ‡aStrains and stresses. |
| 650 | ⊔ | 0 | ‡aMatrices. |
| 650 | ⊔ | 0 | ‡aComputer programming. |
| 650 | ⊔ | 0 | ‡aShells (Engineering) |
| 700 | 1 | ⊔ | ‡aJordan, Stephen, ‡eauthor. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡eissuing agency. |
| 710 | 2 | ⊔ | ‡aBell Aerospace Textron, ‡esponsor. |
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