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The effects of horizontal-tail height and a partial-span leading-edge extension on the static longitudinal stability of a wing-fuselage-tail combination having a sweptback wing
| Content Provider | Semantic Scholar |
|---|---|
| Author | Bandettini, Angelo Selan, Ralph |
| Copyright Year | 1954 |
| Abstract | Memorandum presenting an investigation made to valuate the effects of vertical height of the horizontal tail on the static longitudinal stability of a model with a wing with 35 degrees of sweepback, an aspect ratio of 4.5, a taper ratio of 0.5, and NACA 64A010 sections. The investigation also included the effects of adding a partial-span, leading-edge chord extension to the outer portions of the wing. Results regarding the effect of tail height, wing-wake and local downwash measurements, and effect of a leading-edge extension are provided. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | https://digital.library.unt.edu/ark:/67531/metadc60558/m2/1/high_res_d/19930088273.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |