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Low-speed wind-tunnel tests of a 1/10-scale model of an advanced arrow-wing supersonic cruise configuration designed for cruise at mach 2.2. [langley full scale wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Yip, L. P. |
| Copyright Year | 1979 |
| Description | The low-speed longitudinal and lateral-directional characteristics of a scale model of an advanced arrow-wing supersonic cruise configuration were investigated in tests conducted at a Reynolds number of 4.19 x 10 to the 6th power based on the mean aerodynamic chord, with an angle of attack range from - 6 deg to 23 deg and sideslip angle range from -15 deg to 20 deg. The effects of segmented leading-edge flaps, slotted trailing-edge flaps, horizontal and vertical tails, and ailerons and spoilers were determined. Extensive pressure data and flow visualization pictures with non-intrusive fluorescent mini-tufts were obtained. |
| File Size | 40688622 |
| Page Count | 265 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800001896 |
| Archival Resource Key | ark:/13960/t2m669v63 |
| Language | English |
| Publisher Date | 1979-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Scale Models Supersonic Cruise Aircraft Research Low Speed Pressure Distribution Spoilers Tables Data Arrow Wings Wind Tunnel Tests Flaps Control Surfaces Flow Visualization Trailing Edge Flaps Aerodynamic Characteristics Leading Edges Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
