Ground Effect Vehicles - Presentation 2 - Screen 12 on FlowVella - Presentation Software for Mac iPad and iPhone

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Theory of GEV’s

Peter

Lift : Angle of Attack

- Angle of attack to be between 9 degrees and 18 degrees

Figure 4 : Flow pattern on suction surface of a wing in ground effect

Figure 5 : Lift coefficient against angle of attack for a Tryrell-26 wing in ground effect

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Ground Effect Vehicles - Presentation 2

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