left-click = rotate, middle-button/CTLR-left-click = pan, scroll/right-click/ALT-left-click = zoom
| File ID# | 262 |
| Units | Meters |
| Description | Concept suggestion for swept wing flight control in pitch and roll with variable winglet toe out; Under study: whether associated yaw moments are favorable during roll; Reduced empennage for reduced drag; active yaw control with ventral canard; Main canards, usually floating, are activated only for takeoff rotation or emergency supplementary pitch control |
| Source Quality |
3 - The source material used to create this model was Good. This means good 3-view drawings were used to create the model.
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| Model Suitability |
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| Tags |
airliner
,
general aviation
,
airplane
,
military
,
engine
,
flaps
|