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Static aerodynamic characteristics of a model with a 17 percent thick supercritical wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ferris, J. C. |
| Copyright Year | 1972 |
| Description | The statis stability and control characteristics and air loads on the wing and aileron of a 0.09 scale model of an airplane with a 17 percent thick supercritical wing were investigated. The longitudinal aerodynamic characteristics were determined over a lift coefficient range sufficiently high to induce buffet onset at Mach numbers from 0.30 to 0.80. In addition, the lateral aerodynamic characteristics were determined as a function of sideslip angle and angle of attack at selected Mach numbers. |
| File Size | 31659672 |
| Page Count | 144 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830002804 |
| Archival Resource Key | ark:/13960/t07x15092 |
| Language | English |
| Publisher Date | 1972-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Static Stability Lateral Stability Ailerons Aerodynamic Stability Longitudinal Stability Sideslip Lift Aircraft Models Thickness Wind Tunnel Tests Supercritical Wings Wing Profiles Angle of Attack Buffeting Aerodynamic Loads 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 |
