Propeller Slipstream & Tailplane Instability

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The impact of propeller slipstream on tailplane stability is significant, particularly for aircraft with tractor propellers, potentially necessitating dual rudders to counteract the effects. The slipstream creates a sidewash that alters the vertical fin's angle of attack, complicating control. Computational Fluid Dynamics (CFD) can be used to visualize the helix path, but this approach demands extensive processing power and resources. The complexity of the aircraft design plays a crucial role in determining the extent of instability caused by the slipstream. Understanding these dynamics is essential for effective aircraft design and control.
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Is the effect that the propeller slipstream (i.e the helix) hits the tailplane causing much instability quite significant such that if u are using a tractor propeller a single rudder won't work creating the need for two rudders away from the slipstream path??
 
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There is no easy answer to that question, as it depends on the design of the aircraft. The effect of the slipstream is to induce a sidewash factor that modifies the verticle fins angle of attack.
 
Is there any way to actually find the path of the helix?...like using CFD.
 
Sure, you can run CFD and then look at a plot of the streamlines. But that is going to be a huge under taking, and require a ton of processing power.
 
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