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Low-speed aerodynamic characteristics of a model having a 42 deg swept low wing with a supercritical airfoil, double-slotted flaps, and a t-tail
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sleeman Jr., W. C. Fournier, P. G. |
| Copyright Year | 1972 |
| Description | A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static longitudinal and lateral stability characteristics of a general research model which simulated an advance configuration for a commercial transport airplane with a T tail. The model had a 42 deg swept, aspect ratio 6.78 wing with a supercritical airfoil and a high lift system which consisted of a leading edge slat and a double slotted flap. Various slat and flap deflection combinations represented clean, take off, and landing configurations. Effects on the longitudinal and lateral aerodynamic characteristics were determined for two flow through, simulated engine nacelles located on the sides of the fuselage near the rear of the model. |
| File Size | 23895018 |
| Page Count | 65 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830002760 |
| Archival Resource Key | ark:/13960/t5dc2sv9h |
| Language | English |
| Publisher Date | 1972-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aeronautics (general) Low Speed Stability Slots Swept Wings Transport Aircraft Leading Edge Slats Supercritical Wings Wind Tunnel Models T Tail Surfaces Low Speed Wind Tunnels Aerodynamic Characteristics Aircraft Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
