| LDR | 01174cam a2200253 a 4500 | ||
| 001 | 011427872 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 830117s1982 dcua b f00010 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc68536 |
| 035 | ⊔ | ⊔ | ‡9AAH-4292 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)9135483 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dUIU |
| 074 | ⊔ | ⊔ | ‡a830-H-15 (microfiche) |
| 086 | 0 | ⊔ | ‡aNAS 1.60:2012 |
| 100 | 1 | 0 | ‡aBarger, Raymond L. |
| 245 | 1 | 3 | ‡aAn Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations / ‡cRaymond L. Barger. |
| 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], ‡c1982. |
| 490 | ⊔ | 0 | ‡aNASA technical paper. ‡v2012 |
| 500 | ⊔ | ⊔ | ‡a"Langley Research Center." |
| 500 | ⊔ | ⊔ | ‡a"May 1982"--Cover. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings |
| 710 | 2 | 0 | ‡aLangley Research Center. |
| 710 | 1 | 0 | ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch. |
| CID | ⊔ | ⊔ | ‡a011427872 |
| DAT | 0 | ⊔ | ‡a20020415161319.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2025-01-01T18:38:07Z |
| DAT | 2 | ⊔ | ‡a2025-01-01T18:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20250101 ‡sgoogle ‡uuiug.30112101593892 ‡y1982 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019 |