Loading...
Please wait, while we are loading the content...
Similar Documents
The nasa langley laminar-flow-control experiment on a swept, supercritical airfoil: evaluation of initial perforated configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stack, John P. Harris, Charles D. Brooks Jr., Cuyler W. Clukey, Patricia G. |
| Copyright Year | 1992 |
| Description | The initial evaluation of a large-chord, swept, supercritical airfoil incorporating an active laminar-flow-control (LFC) suction system with a perforated upper surface is documented in a chronological manner, and the deficiencies in the suction capability of the perforated panels as designed are described. The experiment was conducted in the Langley 8-Foot Transonic Pressure Tunnel. Also included is an evaluation of the influence of the proximity of the tunnel liner to the upper surface of the airfoil pressure distribution. |
| File Size | 6463236 |
| Page Count | 126 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920012953 |
| Archival Resource Key | ark:/13960/t0tr0tj79 |
| Language | English |
| Publisher Date | 1992-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Suction Transonic Flow Laminar Boundary Layer Swept Wings Laminar Flow Transonic Wind Tunnels Wind Tunnel Tests Pressure Distribution Supercritical Wings Airfoils Boundary Layer Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
