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Low speed wind tunnel tests of a 1/9-scale model of a variable-sweep advanced supersonic transport
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McLemore, H. C. Sewall, W. G. Parlett, L. P. |
| Copyright Year | 1974 |
| Description | Tests have been conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics of a 1/9-scale variable-sweep advanced supersonic transport configuration. The model configurations investigated were the basic unflapped arrangement, and a takeoff and landing flap arrangement with several strake leading edge flow control devices. The tests were conducted for an angle-of-attack range from about minus 5 deg to 36 deg and a sideslip range from minus 5 deg to 10 deg. The tests were conducted for a range of Reynolds number from 3.92 million to 5.95 million corresponding to test velocities of about 54.5 knots and 81.7 knots, respectively. |
| File Size | 3302178 |
| Page Count | 86 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740018344 |
| Archival Resource Key | ark:/13960/t59d1qc03 |
| Language | English |
| Publisher Date | 1974-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Aircraft Stability Aerodynamic Configurations Variable Sweep Wings Data Acquisition Technology Transfer Low Speed Wind Tunnel Tests Data Processing Aircraft Design Supersonic Transports Aerodynamic Characteristics Aircraft Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
