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Wind tunnel tests of a full-scale model of a light twin-engine airplane with fixed auxiliary airfoil or leading-edge slot
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fink, M. P. Shivers, J. P. White, L. C. |
| Copyright Year | 1974 |
| Description | An investigation has been conducted by means of wind-tunnel tests of a full-scale mockup of a light twin-engine airplane configuration to determine the effects of outboard partial-span slots and of auxiliary airfoils ahead of the leading edge of the wing in improving aerodynamic characteristics at high angles of attack. Both of the stall-control devices gave considerable improvement in high angle-of-attack characteristics with the auxiliary airfoil giving the more favorable results, but neither device performed as well as might have been expected. |
| File Size | 4010320 |
| Page Count | 119 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740011552 |
| Archival Resource Key | ark:/13960/t81k45s5g |
| Language | English |
| Publisher Date | 1974-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Aerodynamic Configurations Data Acquisition Wind Tunnel Tests Airfoils Wing Slots Aerodynamic Characteristics Light Aircraft Aerodynamic Stalling Leading Edges Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
