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Future transport with variable winglet toe

left-click = rotate, middle-button/CTLR-left-click = pan, scroll/right-click/ALT-left-click = zoom

Downloads: 765
Uploaded by: J. Philip Barnes
File size: 59 kilobytes
VSP Version: 2.X
License: Public Domain

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.

Model Suitability
  • 5 - Build a display model
  • 5 - Cartoon or Pretty Picture
Tags airliner , general aviation , airplane , military , engine , flaps

Enter all tags that describe the file separated by commas. (i.e. "Part, Engine, Aircraft")


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