| LDR | 01323cam a2200301Ia 4500 | ||
| 001 | 011428067 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 810819s1981 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6370639 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)7680632 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dABC |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3 ‡b.N18 no. 1881 |
| 074 | ⊔ | ⊔ | ‡a830-H-15 (microfiche) |
| 086 | 0 | ⊔ | ‡aNAS 1.60:1881 |
| 100 | 1 | ⊔ | ‡aBarger, Raymond L. |
| 245 | 1 | 2 | ‡aA procedure for designing forebodies with constraints on cross-section shape and axial area distribution / ‡cRaymond L. Barger. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1981. |
| 300 | ⊔ | ⊔ | ‡a12 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical paper ; ‡vno. 1881 |
| 500 | ⊔ | ⊔ | ‡a"Langley Research Center." |
| 500 | ⊔ | ⊔ | ‡a"July 1981"--Cover. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aGuided missiles ‡xDesign and construction. |
| 650 | ⊔ | 0 | ‡aSupersonic planes ‡xDesign and construction. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch. |
| CID | ⊔ | ⊔ | ‡a011428067 |
| DAT | 0 | ⊔ | ‡a20101013103137.0 ‡b20141013010000.0 |
| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2025-01-01T19:25:36Z |
| DAT | 2 | ⊔ | ‡a2025-01-01T18:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6370639 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106670844 ‡sUIU ‡16370639 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20250101 ‡sgoogle ‡uuiug.30112106670844 ‡y1981 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019 |