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Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds
| Content Provider | University of North Texas |
|---|---|
| Author | Malvestuto, Frank S. Jr. Hoover, Dorothy M. |
| Organization | Langley Aeronautical Laboratory |
| Description | Note presenting the lift-due-to-pitching derivative and the damping-in-pitch derivative, which were derived for a series of thin sweptback tapered wings with streamwise tips and subsonic leading edges. The effects of camber and thickness were not considered. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc55650 |
| Language | English |
| Publisher Date | 2018-11-26 |
| Access Restriction | Open |
| Subject Keyword | thin sweptback wings supersonic flow theory |
| Content Type | Text |
| Resource Type | Report |