| LDR | 01342nam a2200337Ia 4500 | ||
| 001 | 011433059 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 931116s1975 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6390062 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)29335647 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cABC |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521 ‡b.A3525 no. 7935 |
| 100 | 1 | ⊔ | ‡aAnderson, James Kent. |
| 245 | 1 | 0 | ‡aBuckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure / ‡cJames Kent Anderson and Randall C. Davis. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1975. |
| 300 | ⊔ | ⊔ | ‡a99 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vNASA TN D-7935 |
| 500 | ⊔ | ⊔ | ‡aPrepared at Langley Research Center. |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 14). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aSandwich construction. |
| 650 | ⊔ | 0 | ‡aHoneycomb structures. |
| 650 | ⊔ | 0 | ‡aShells (Engineering) |
| 650 | ⊔ | 0 | ‡aBuckling (Mechanics) |
| 650 | ⊔ | 0 | ‡aAluminum ‡xMechanical properties. |
| 650 | ⊔ | 0 | ‡aMaterials ‡xCompression testing. |
| 700 | 1 | ⊔ | ‡aDavis, Randall C. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| CID | ⊔ | ⊔ | ‡a011433059 |
| DAT | 0 | ⊔ | ‡a20101101134143.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2024-03-23T18:07:59Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6390062 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106632570 ‡sUIU ‡16390062 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240323 ‡sgoogle ‡uuiug.30112106632570 ‡y1975 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019 |