| LDR | 01030cam a2200241Ia 4500 | ||
| 001 | 011447799 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 030611s1967 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6392826 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)52412706 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cEGM ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aSewall, John L. |
| 245 | 1 | 0 | ‡aVibration analysis of cylindrically curved panels with simply supported or clamped edges and comparison with some experiments / ‡cJohn L. Sewall. |
| 246 | 3 | ⊔ | ‡aNASA TN D-3791 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], ‡c1967. |
| 300 | ⊔ | ⊔ | ‡a48 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-3791 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 31-32). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aCurvature. |
| 650 | ⊔ | 0 | ‡aVibration. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011447799 |
| DAT | 0 | ⊔ | ‡a20101103103829.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:21:34Z |
| DAT | 2 | ⊔ | ‡a2023-03-14T17:30:02Z ‡b2020-08-29T20:00:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6392826 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106634733 ‡sUIU ‡16392826 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106634733 ‡y1967 ‡rpdus ‡qgfv |