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Low-speed wind tunnel tests of 1/9-scale model of a variable-sweep supersonic cruise aircraft. [conducted in the langley full-scale wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McLemore, H. C. Sewall, W. G. Parlett, L. P. |
| Copyright Year | 1977 |
| Description | Tests were conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics at low subsonic speeds of a 1/9-scale model of a variable-sweep supersonic cruise aircraft. The model configurations investigated were the basic unflapped arrangement, a take-off flap arrangement, and a landing flap arrangement with several strake leading-edge flow control devices. The tests were conducted at angles of attack from about -5 to 36 deg, sideslip angles from -5 to 10 deg. |
| File Size | 3513263 |
| Page Count | 82 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770019126 |
| Archival Resource Key | ark:/13960/t89h0fk3d |
| Language | English |
| Publisher Date | 1977-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aeronautics (general) Supersonic Aircraft Variable Sweep Wings Scale Models Wind Tunnel Tests Low Speed Wind Tunnels Angle of Attack Aerodynamic Characteristics 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 |
