| LDR | 02828cam a2200385Ia 4500 | ||
| 001 | 011425157 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 050930s1986 dcua b f000 0 eng d | ||
| 024 | 8 | ⊔ | ‡aN8818567 |
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6361065 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)61748296 |
| 040 | ⊔ | ⊔ | ‡aFER ‡cFER ‡dFER |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.60:2619 |
| 088 | ⊔ | ⊔ | ‡aH-1193 |
| 100 | 1 | ⊔ | ‡aMeyer, Robert R., ‡cJr. |
| 245 | 1 | 0 | ‡aEffects of winglets on a first-generation jet transport wing. ‡nVII, ‡pSideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model / ‡cRobert R. Meyer, Jr., and Peter F. Covell. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1986. |
| 300 | ⊔ | ⊔ | ‡a56 p. : ‡bill. ; ‡c28 cm. ‡e+ 7 microfiches |
| 490 | ⊔ | 0 | ‡aNASA technical paper ; ‡v2619 |
| 500 | ⊔ | ⊔ | ‡aAccession ID: 88N18567. |
| 500 | ⊔ | ⊔ | ‡aDocument ID: 19880009183. |
| 500 | ⊔ | ⊔ | ‡aTable 4, "Low-Speed Winglet Pressure Data," and Table 5, "High-Speed Wing and Winglet Pressure Data" are provided in the microfiche supplement (7 fiche) included in this report. |
| 500 | ⊔ | ⊔ | ‡a"September 1986." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 11). |
| 520 | ⊔ | ⊔ | ‡a"The effect of sideslip on winglet loads and selected wing loads was investigated at high and low subsonic Mach numbers. The investigation was conducted in two separate wind tunnel facilities, using two slightly different 0.035-scale full-span models. Results are presented which indicate that, in general, winglet loads as a result of sideslip are analogous to wing loads caused by angle of attack. The center-of-pressure locations on the winglets are somewhat different than might be expected for an analogous wing. The spanwise center of pressure for a winglet tends to be more inboard than for a wing. The most notable chordwise location is a forward center-of-pressure location on the winglet at high sideslip angles. The noted differences between a winglet and an analogous wing are the result of the influence of the wing on the winglet."--Technical report documentation page. |
| 530 | ⊔ | ⊔ | ‡aAlso available online in PDF from NASA Technical Reports Server. |
| 536 | ⊔ | ⊔ | ‡aSponsored by National Aeronautics and Space Administration; performed by NASA Ames Research Center, Dryden Flight Research Center, Edwards, Calif. ‡dRTOP 505-31-21 |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamic load. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings. |
| 700 | 1 | ⊔ | ‡aCovell, Peter F. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011425157 |
| DAT | 0 | ⊔ | ‡a20101005090707.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2023-03-14T18:19:57Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6361065 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106613679 ‡sUIU ‡16361065 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106613679 ‡y1986 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |