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Two-dimensional wind-tunnel tests of a nasa supercritical airfoil with various high-lift systems. volume 1: data analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zierten, T. Omar, E. Mahal, A. |
| Copyright Year | 1977 |
| Description | High-lift systems for a NASA, 9.3%, method for calculating the viscous flow about two-dimensional multicomponent airfoils was evaluated by comparing its predictions with test data. High-lift systems derived from supercritical airfoils were compared in terms of performance to high-lift systems derived from conventional airfoils. The high-lift systems for the supercritical airfoil were designed to achieve maximum lift and consisted of: a single-slotted flap; a double-slotted flap and a leading-edge slat; and a triple-slotted flap and a leading-edge slat. Agreement between theoretical predictions and experimental results are also discussed. |
| File Size | 3147648 |
| Page Count | 91 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800003804 |
| Archival Resource Key | ark:/13960/t3jx35h8p |
| Language | English |
| Publisher Date | 1977-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Two Dimensional Boundary Layer Leading Edge Slats Wind Tunnel Tests Wakes Supercritical Wings Airfoils Boundary Layer Control Lift Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
