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Formulas and Charts for the Supersonic Lift and Drag of Flat Swept-Back Wings With Interacting Leading and Trailing Edges
| Content Provider | University of North Texas |
|---|---|
| Author | Cohen, Doris |
| Organization | Ames Aeronautical Laboratory (U.S.) |
| Description | Note presenting formulas and design charts for the lift in cases for wings with rectilinear plan forms swept so that both leading and trailing edges lie within their respective Mach cones. The charts cover a practical range of aspect ratios and plan forms of moderate taper, with tips parallel to the stream. Numerical results and an application of the charts are included. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc55632 |
| Language | English |
| Publisher Date | 2018-10-29 |
| Access Restriction | Open |
| Subject Keyword | lift characteristics drag characteristics aircraft wings |
| Content Type | Text |
| Resource Type | Report |