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Effects of Horizontal-Tail Position and a Wing Leading-Edge Modification Consisting of a Full-Span Flap and a Partial-Span Chord-Extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model With a 45 Degree Sweptback Wing
| Content Provider | University of North Texas |
|---|---|
| Author | Morrison, William D. Jr. Alford, William J. Jr. |
| Organization | Langley Aeronautical Laboratory |
| Description | Note presenting an investigation conducted in the high-speed 7- by 10-foot tunnel to determine the effects of varying the horizontal-tail position relative to the wing chord plane on the aerodynamic characteristics in pitch of a general research model having a 45 degree sweptback wing of aspect ratio 4, taper ratio 0.30, and NACA 65A006 airfoil sections. The investigation also included the effects of a wing modification consisting of a full-span leading-edge flap deflected 6 degrees and an outboard partial-span chord-extension. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc56280 |
| Language | English |
| Publisher Date | 2018-11-29 |
| Access Restriction | Open |
| Subject Keyword | aerodynamics sweptback wings |
| Content Type | Text |
| Resource Type | Report |
