| LDR | 01123cam a2200265Ia 4500 | ||
| 001 | 011433481 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 040806s1965 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6391153 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)56103526 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cEGM ‡dOCLCQ ‡dKLG |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | 1 | 4 | ‡aTL521 ‡b.A3525 no.2243 |
| 100 | 1 | ⊔ | ‡aGrantham, William D. |
| 245 | 1 | 0 | ‡aEffects of aircraft relative density on spin and recovery characteristics of some current configurations / ‡cWilliam D. Grantham and Sue B. Grafton. |
| 246 | 3 | ⊔ | ‡aNASA TN D-2243 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230], ‡c1965. |
| 300 | ⊔ | ⊔ | ‡a38 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-2243 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 15). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aSpin (Aerodynamics) ‡xTesting. |
| 700 | 1 | ⊔ | ‡aGrafton, Sue B. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011433481 |
| DAT | 0 | ⊔ | ‡a20101102100822.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2024-01-23T18:45:17Z |
| DAT | 2 | ⊔ | ‡a2024-01-23T18:30:02Z ‡b2020-08-29T20:00:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6391153 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106866186 ‡sUIU ‡16391153 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240123 ‡sgoogle ‡uuiug.30112106866186 ‡y1965 ‡rpdus ‡qgfv |