| LDR | 01262cam a2200301Ia 4500 | ||
| 001 | 011425338 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 070815s1977 dcua b 000 0 eng d | ||
| 029 | 1 | ⊔ | ‡aGBVCP ‡b60924454X |
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6361465 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)164564755 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cEGM |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aKaufman, Louis G., ‡cII. |
| 245 | 1 | 0 | ‡aPressure distributions induced by elevon deflections on swept wings and adjacent end-plate surfaces at Mach 6 / ‡cLouis G. Kaufman II, Charles B. Johnson. |
| 246 | 3 | ⊔ | ‡aNASA TM X-3470 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡aSpringfield, VA : ‡bFor sale by the Clearinghouse for Federal Scientific and Technical Information, ‡c1977. |
| 300 | ⊔ | ⊔ | ‡a122 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical memorandum ; ‡vX-3470 |
| 500 | ⊔ | ⊔ | ‡aPrepared by Langley Research Center, Hampton, VA 23665. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 13-14). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings ‡xTesting. |
| 650 | ⊔ | 0 | ‡aWind-pressure. |
| 650 | ⊔ | 0 | ‡aSurfaces. |
| 700 | 1 | ⊔ | ‡aJohnson, Charles B. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011425338 |
| DAT | 0 | ⊔ | ‡a20101005113625.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2024-01-17T02:05:20Z |
| DAT | 2 | ⊔ | ‡a2024-01-16T18:30:02Z ‡b2022-09-29T20:00:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6361465 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106562975 ‡sUIU ‡16361465 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240117 ‡sgoogle ‡uuiug.30112106562975 ‡y1977 ‡rpdus ‡qgfv |