| LDR | 01207cam a2200277Ia 4500 | ||
| 001 | 011446272 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 030718s1966 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6405244 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)52638532 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cEGM ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aSpreemann, Kenneth P. |
| 245 | 1 | 0 | ‡aWind-tunnel investigation of longitudinal aerodynamic characteristics of a powered four-duct-propeller VTOL model in transition / ‡cKenneth P. Spreemann. |
| 246 | 3 | ⊔ | ‡aNASA TN D-3192 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], ‡c1966. |
| 300 | ⊔ | ⊔ | ‡a125 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-3192 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 10). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aRocket engines ‡xThrust. |
| 650 | ⊔ | 0 | ‡aWind tunnels. |
| 650 | ⊔ | 0 | ‡aSpace shuttles ‡xLongitudinal stability. |
| 650 | ⊔ | 0 | ‡aVertically rising aircraft ‡xAerodynamics. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| CID | ⊔ | ⊔ | ‡a011446272 |
| DAT | 0 | ⊔ | ‡a20101111095728.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2024-01-26T18:53:13Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240126 ‡sgoogle ‡uuiug.30112106599167 ‡y1966 ‡ric ‡qbib ‡tUS bib date1 >= 1929 |