| LDR | 01437cam a2200313Ii 4500 | ||
| 001 | 011426010 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 760706s1976 dcua b f000 0 eng d | ||
| 029 | 1 | ⊔ | ‡aGBVCP ‡b609127896 |
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6363357 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)2298364 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dOCL ‡dABC ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3.T4 ‡bA3 no. 3376 |
| 086 | 0 | ⊔ | ‡aNAS 1.15:X-3376 |
| 100 | 1 | ⊔ | ‡aBlair, A. B. |
| 245 | 1 | 0 | ‡aEffect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ̊clipped-delta-wing orbiter configuration at supersonic mach numbers / ‡cA.B. Blair, Jr. ; Langley Research Center, Hampton, Va. |
| 260 | ⊔ | ⊔ | ‡aWashington : ‡bU.S. National Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1976. |
| 300 | ⊔ | ⊔ | ‡a[1], 95 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical memorandum ; NASA TM X-3376 |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 9). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aStability of space vehicles. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings, Triangular. |
| 650 | ⊔ | 0 | ‡aAerodynamics, Supersonic. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| CID | ⊔ | ⊔ | ‡a011426010 |
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| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2025-01-01T19:14:54Z |
| DAT | 2 | ⊔ | ‡a2025-01-01T18:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6363357 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112105196122 ‡sUIU ‡16363357 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20250101 ‡sgoogle ‡uuiug.30112105196122 ‡y1976 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019 |