| LDR | 02952cam a2200421Ia 4500 | ||
| 001 | 011449852 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 040527s1970 dcua bt f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6405304 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)249597047 |
| 040 | ⊔ | ⊔ | ‡aGyGoGBV ‡erakwb ‡bger ‡cGBVCP ‡dFER |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-7031 |
| 090 | ⊔ | ⊔ | ‡aTL672 |
| 100 | 1 | ⊔ | ‡aHodder, Brent K. |
| 245 | 1 | 0 | ‡aAerodynamic characteristics of a large-scale model a lift fan mounted in a 5-percent-thick triangular wing, including the effects of BLC on the lift-fan inlet / ‡cBrent K. Hodder, Jerry V. Kirk, and Leo P. Hall. |
| 260 | ⊔ | ⊔ | ‡aWashington, DC : ‡bNational Aeronautics and Space Administration, ‡c1970. |
| 300 | ⊔ | ⊔ | ‡aiv, 52 p. : ‡bill. ; ‡c26 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vNASA TN D-7031 |
| 500 | ⊔ | ⊔ | ‡a"A-2822." |
| 500 | ⊔ | ⊔ | ‡a"NASA TN D-7031." |
| 500 | ⊔ | ⊔ | ‡a"December 1970." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 10). |
| 520 | ⊔ | ⊔ | ‡aThe low-speed aerodynamics of a large-scale triangular wing model, with a reduced thickness, tip-turbine driven lift fan in each wing were investigated in the Ames 40-by 80-Foot Wind Tunnel. The model had a 5-percent-thick wing typical of wings designed for supersonic performance.Conventional lift-fan depth has, in the past, limited wing thickness to about 10 percent. A thinner lift fan for the present investigation was obtained by modification of a conventional fan. The modification included removing the discharge stator and reducing the fan inlet length and radius. To control airflow separation resulting from small inlet radii, blowing boundary-layer control was applied through a nozzle in the inlet. Performance of the modified fan along with aerodynamic characteristics of the total configuration is presented. The static thrust performance of the conventional fan (requiring a lo-percent wing) was equalled by the reduced thickness fans of this investigation.--P. [i]. |
| 530 | ⊔ | ⊔ | ‡aAlso available online in PDF from NASA Technical Reports Server Web site. |
| 536 | ⊔ | ⊔ | ‡aSponsored by the National Aeronautics and Space Administration (NASA); performed by the NASA Ames Research Center and the U.S. Army Air Mobility Research and Development Laboratory under ‡h721-01-00-05-00-21. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamics. |
| 650 | ⊔ | 0 | ‡aBoundary layer control. |
| 650 | ⊔ | 0 | ‡aFan-in-wing aircraft ‡xEvaluation. |
| 700 | 1 | ⊔ | ‡aHall, Leo P. |
| 700 | 1 | ⊔ | ‡aKirk, Jerry V. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| 710 | 2 | ⊔ | ‡aU.S. Army Air Mobility Research and Development Laboratory. |
| 710 | 2 | ⊔ | ‡aAmes Research Center. |
| CID | ⊔ | ⊔ | ‡a011449852 |
| DAT | 0 | ⊔ | ‡a20101111101116.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2025-01-02T19:06:45Z |
| DAT | 2 | ⊔ | ‡a2025-01-02T18:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6405304 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106748376 ‡sUIU ‡16405304 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20250102 ‡sgoogle ‡uuiug.30112106748376 ‡y1970 ‡rpd ‡qbib ‡tUS fed doc |