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Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Walker, Charlotte E. Bennett, Robert M. |
| Copyright Year | 1999 |
| Description | Proposed computational test cases have been selected from the data set for a rectangular wing of panel aspect ratio two with a twelve-percent-thick supercritical airfoil section that was tested in the NASA Langley Transonic Dynamics Tunnel. The test cases include parametric variation of static angle of attack, pitching oscillation frequency, and Mach numbers from subsonic to transonic with strong shocks. Tables and plots of the measured pressures are presented for each case. This report provides an early release of test cases that have been proposed for a document that supplements the cases presented in AGARD Report 702. |
| File Size | 4660988 |
| Page Count | 132 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19990036167 |
| Archival Resource Key | ark:/13960/t2k69dr2w |
| Language | English |
| Publisher Date | 1999-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Static Pressure Transonic Flow Subsonic Speed Computational Fluid Dynamics Transonic Wind Tunnels Rectangular Wings Aircraft Parts Aspect Ratio Airfoil Profiles Wing Oscillations Unsteady Aerodynamics Wind Tunnel Tests Supercritical Wings Angle of Attack 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 |
