| LDR | 01160cam a2200301Ia 4500 | ||
| 001 | 100233513 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 091105s1959 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6362944 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)463402076 |
| 040 | ⊔ | ⊔ | ‡aCSL ‡cTEF |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL673.S9 ‡bM84 1959 |
| 100 | 1 | ⊔ | ‡aMueller, James N. |
| 245 | 1 | 0 | ‡aEffects of twist and camber and thickness on the aerodynamic characteristics of a 75° swept arrow wing at a mach number of 2.91 / ‡cby James N. Mueller and John E. Grimaud. |
| 260 | ⊔ | ⊔ | ‡aWashington [D.C.] : ‡bNational Aeronautics and Space Administration, ‡c[1959] |
| 300 | ⊔ | ⊔ | ‡a67 p. : ‡b22 ill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical memorandum ; ‡vX-138 |
| 500 | ⊔ | ⊔ | ‡a"December 1959." |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 18-20). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aCamber (Aerofoils) |
| 650 | ⊔ | 0 | ‡aAerodynamic load. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings, Swept-back. |
| 700 | 1 | ⊔ | ‡aGrimaud, John E. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a100233513 |
| DAT | 0 | ⊔ | ‡a20101006114332.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2024-01-24T18:36:59Z |
| DAT | 2 | ⊔ | ‡a2024-01-24T18:30:02Z ‡b2023-02-25T21:00:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6362944 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106564153 ‡sUIU ‡16362944 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240124 ‡sgoogle ‡uuiug.30112106564153 ‡y1959 ‡rpdus ‡qncn |