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Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Oliver, W. R. Allen, J. B. Spacht, L. A. |
| Copyright Year | 1982 |
| Description | The wind tunnel testing of an advanced technology high lift system for a wide body and a narrow body transport incorporating high aspect ratio supercritical wings is described. This testing has added to the very limited low speed high Reynolds number data base for this class or aircraft. The experimental results include the effects on low speed aerodynamic characteristics of various leading and trailing edge devices, nacelles and pylons, ailerons, and spoilers, and the effects of Mach and Reynolds numbers. |
| File Size | 7674381 |
| Page Count | 189 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840020673 |
| Archival Resource Key | ark:/13960/t4qk27t53 |
| Language | English |
| Publisher Date | 1982-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Slender Wings Aerodynamic Configurations Transport Aircraft Reynolds Number Wind Tunnel Tests Ailerons Supercritical Wings Nacelles Wind Tunnel Models Aerodynamic Characteristics Pylons Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
