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| 001 | 011426515 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
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| 007 | cr bn ---auaua | ||
| 008 | 780606s1977 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6365262 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)3953275 |
| 037 | ⊔ | ⊔ | ‡b22161 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dOCL ‡dABC ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3 ‡b.N18 no. 1070 |
| 074 | ⊔ | ⊔ | ‡a830-H-15 (microfiche) |
| 086 | 0 | ⊔ | ‡aNAS 1.60:1070 |
| 100 | 1 | ⊔ | ‡aWilmoth, Richard G. |
| 245 | 1 | 0 | ‡aComputation of transonic boattail flow with separation / ‡cRichard G. Wilmoth. |
| 260 | ⊔ | ⊔ | ‡a[Washington] : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1977. |
| 300 | ⊔ | ⊔ | ‡a63 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical paper ; ‡v1070 |
| 500 | ⊔ | ⊔ | ‡aIssued Dec. 1977. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aDrag (Aerodynamics) |
| 650 | ⊔ | 0 | ‡aBase flow (Aerodynamics) |
| 650 | ⊔ | 0 | ‡aJet nozzles. |
| 650 | ⊔ | 0 | ‡aAerodynamics, Transonic. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office. |
| CID | ⊔ | ⊔ | ‡a011426515 |
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| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2023-03-14T18:23:23Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106664631 ‡y1977 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |