| LDR | 01247cam a2200301Ma 4500 | ||
| 001 | 011443567 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 041209s1971 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6402013 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)647938433 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cSTF |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-6100 |
| 088 | ⊔ | ⊔ | ‡aNASA-TN-D-6100 |
| 100 | 1 | ⊔ | ‡aAdelman, Howard M. |
| 245 | 1 | 0 | ‡aCalculation of temperature distributions in thin shells of revolution by the finite-element method / ‡cHoward M. Adelman and Donnell S. Catherines. |
| 246 | 3 | ⊔ | ‡aNASA TN D-6100 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], ‡c1971. |
| 300 | ⊔ | ⊔ | ‡a52 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vD-6100 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 52). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aFinite element method. |
| 650 | ⊔ | 0 | ‡aShells (Engineering) ‡xThermal properties. |
| 700 | 1 | ⊔ | ‡aCatherines, Donnell S. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011443567 |
| DAT | 0 | ⊔ | ‡a20101109145631.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:35:53Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6402013 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106880419 ‡sUIU ‡16402013 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106880419 ‡y1971 ‡rpd ‡qbib ‡tUS fed doc |