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A Preliminary Low-Speed Wind-Tunnel Investigation of a Thin Delta Wing Equipped With a Double and a Single Slotted Flap
| Content Provider | University of North Texas |
|---|---|
| Author | MacLeod, Richard G. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting a low-speed wind-tunnel investigation to determine the high-lift characteristics of a thin delta wing equipped with a single and double slotted trailing edge flap. Results regarding the lift, drag, and pitching-moment characteristics of the plain wing and various flap configurations are provided. The maximum lift coefficient of the model could be increased from 1.45 for the plain wing to 1.86 when the double slotted flap was deflected to 50 degrees. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc58963 |
| Language | English |
| Publisher Date | 2019-01-15 |
| Access Restriction | Open |
| Subject Keyword | aircraft wings aircraft flaps aircraft stability |
| Content Type | Text |
| Resource Type | Report |