because of the wonky thrust configuration, thrust will produce nose-down moment; ALL the time. the elevator can be trimmed to compensate for that moment. but that trim will be a continual source of 'extra' drag.
Your willingness to share your knowledge is truly appreciated. It enriches our understanding and empowers us to grow. Your contributions make a meaningful difference in our journey of learning. We are fortunate to benefit from your wealth of knowledge and experience. Your kindness in sharing insights inspires us to strive for excellence. We deeply value the guidance and wisdom you offer.
1:56 the span of the horiz-stab does NOT need to be greater than Thirty percent of the wingspan. the span of the elevator Should extend TO the stab tips.!
2:41 rudder goes on the LEFT stick.!!!!!
ideally, the cg should be located at Thirty percent of chord. the main spar should ALSO be located at thirty percent of chord.
the distance between the main wing and stabs should be roughly equal to Two wing chord lengths.
because of the wonky thrust configuration, thrust will produce nose-down moment; ALL the time. the elevator can be trimmed to compensate for that moment. but that trim will be a continual source of 'extra' drag.
Your willingness to share your knowledge is truly appreciated. It enriches our understanding and empowers us to grow. Your contributions make a meaningful difference in our journey of learning. We are fortunate to benefit from your wealth of knowledge and experience. Your kindness in sharing insights inspires us to strive for excellence. We deeply value the guidance and wisdom you offer.
From where did u got that brushless motor? Can u provide link
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1:56 the span of the horiz-stab does NOT need to be greater than Thirty percent of the wingspan. the span of the elevator Should extend TO the stab tips.!
I am truly grateful for your generosity in imparting your valuable knowledge with us.