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Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line
| Content Provider | University of North Texas |
|---|---|
| Author | Cohen, Doris |
| Organization | Ames Aeronautical Laboratory (U.S.) |
| Description | "The method of superposition of linearized conical flows has been applied to the calculation of the aerodynamic properties, in supersonic flight, of thin flat, swept-back wings at an angle of attack. The wings are assumed to have rectilinear plan forms, with tips parallel to the stream, and to taper in the conventional sense. The investigation covers the moderately supersonic speed range where the Mach lines from the leading-edge apex lie ahead of the wing" (p. 1147). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc60392 |
| Language | English |
| Publisher Date | 2018-10-29 |
| Access Restriction | Open |
| Subject Keyword | sweptback wings flow characteristics |
| Content Type | Text |
| Resource Type | Report |
