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Effect at Transonic Speeds of Inboard Spoilers on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-Body Combination Having a Leading-Edge Chord-Extension
| Content Provider | University of North Texas |
|---|---|
| Author | Henderson, James H. |
| Organization | Langley Aeronautical Laboratory |
| Description | Memorandum presenting an exploratory investigation in the 9- by 12-inch blowdown tunnel to determine the effect of inboard spoilers located along the 20- and 30-percent-chord lines on the static longitudinal stability characteristics of a semispan 45 degree sweptback wing-body combination with a leading-edge chord-extension. The model pitching-moment characteristics were improved by spoilers extending from 15 percent semispan to 45 percent semispan. Results regarding pitching moment, lift, drag, rolling moment, and lateral center of pressure are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc60438 |
| Language | English |
| Publisher Date | 2018-12-04 |
| Access Restriction | Open |
| Subject Keyword | aircraft stability aircraft spoilers |
| Content Type | Text |
| Resource Type | Report |