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Effect of Wing Slats and Inboard Wing Fences on the Longitudinal Stability Characteristics of the Douglas D-558-II Airplane in Accelerated Maneuvers at Subsonic and Transonic Speeds
| Content Provider | University of North Texas |
|---|---|
| Author | Fischel, Jack |
| Organization | Langley Aeronautical Laboratory |
| Description | Memorandum presenting testing of a D-558-II airplane with the wing slats fully extended, with and without inboard wing fences, and with the wing slats half extended and wing fences removed. In order to improve the stick-force characteristics at moderate and large angles of attack, additional tests were conducted with two bungees of differing stiffness alternately attached to the control column. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59977 |
| Language | English |
| Publisher Date | 2018-08-29 |
| Access Restriction | Open |
| Subject Keyword | D-558-II wing slats |
| Content Type | Text |
| Resource Type | Report |