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Aerodynamic characteristics at transonic speeds of a 69 degree delta wing with a triangular plan-form control having a skewed hinge axis and an overhang balance: transonic-bump method
| Content Provider | University of North Texas |
|---|---|
| Author | Wiley, Harleth G. |
| Organization | Langley Aeronautical Laboratory |
| Description | From Introduction: "Presented in this paper are the results of an investigation of a semispan model of a delta wing with 60^o sweepback at the leading edge which was equipped with a large triangular control having an overhang balance mounted on a skewed hinge axis. The purpose of this investigation was to determine the aerodynamic characteristics of a delta wing with a control which was designed to provide aerodynamic balance at zero control deflection based on the span load distribution of reference 1." |
| File Format | |
| Archival Resource Key | ark:/67531/metadc58716 |
| Language | English |
| Publisher Date | 2018-05-15 |
| Access Restriction | Open |
| Subject Keyword | aerodynamics delta wings |
| Content Type | Text |
| Resource Type | Report |
