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Pressure Distribution and Damping in Steady Roll at Supersonic Mach Numbers of Flat Swept-Back Wing with Subsonic Edges
| Content Provider | University of North Texas |
|---|---|
| Author | Walker, Harold J. Ballantyne, Mary B. |
| Organization | Ames Aeronautical Laboratory (U.S.) |
| Description | Note presenting a method for calculating the pressure distribution and damping in steady roll at supersonic Mach numbers of thin, flat, sweptback wings with all edges straight and subsonic. It can be adapted to wings with negative rake at the tips, but the method is developed only for wings with streamwise tips. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc55372 |
| Language | English |
| Publisher Date | 2018-12-06 |
| Access Restriction | Open |
| Subject Keyword | pressure distributions sweptback wings |
| Content Type | Text |
| Resource Type | Report |