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| 001 | 011428010 | ||
| 003 | MiAaHDL | ||
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| 007 | cr bn ---auaua | ||
| 008 | 840228s1983 dcua bt f00010 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc606293 |
| 035 | ⊔ | ⊔ | ‡9ACM-8494 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)10467181 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dUIU |
| 074 | ⊔ | ⊔ | ‡a830-H-15 (microfiche) |
| 086 | 0 | ⊔ | ‡aNAS 1.60:2116 |
| 100 | 1 | 0 | ‡aLeavitt, Laurence D. |
| 245 | 1 | 0 | ‡aEffect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 / ‡cLaurence D. Leavitt. |
| 260 | 0 | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1983. |
| 490 | ⊔ | 0 | ‡aNASA technical paper. ‡v2116 |
| 500 | ⊔ | ⊔ | ‡aDistributed to depository libraries in microfiche. |
| 500 | ⊔ | ⊔ | ‡a"May 1983"--Cover. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aFighter planes ‡xFlight testing |
| 650 | ⊔ | 0 | ‡aAir-engines |
| 710 | 1 | 0 | ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch. |
| CID | ⊔ | ⊔ | ‡a011428010 |
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| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2023-03-14T18:24:05Z |
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| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106670653 ‡y1983 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |