at 14:34, BEFORE worrying about stabilizer Area, the SPAN of the horiz-stab should be Equal to THIRTY percent of wingspan.!!!!!! and, the Height of the vert-stab Should be a bit LESS-than Fifty percent, of THAT.!!!!!! googletranslate
at 18:07, control horns are Not correctly configured.!!! at 18:13, WHY TF did you switch to a ZERO-dihedral wing.?!??!?!?! now, that kind of wing will HAVE to Have, ailerons.!!!!! googletranslate
at 17:38, this graphic is STILL WRONG.!!!!!! 33% is WRONG.!!!!! it is MORE Precise to say that cg SHOULD be located at THIRTY percent of chord.!!!! or, if Desired, a BIT forward of thirty.!!!!! googletranslate
at 11:47, MORE WRONG STUFF.!!!!!!!!!!!! there is a REASON to correctly TAPER a tail boom. and, that tail boom AINT correctly tapered.!!!!!! i have details, if you want them. why does it say " 30 " , at the bottom line.???? yer system for 'measuring' fuselage length LESS-than ideal. specifically, the AFT End of the fuselage Should be considered to be at, the Elevator Trailing Edge.!!!!!!! googletranslate
at 8:55, servos do NOT go aft of the cg.!!!!!!! servos do NOT go aft of the cg.!!!!!!! servos do NOT go aft of the cg.!!!!!!! servos do NOT go aft of the cg.!!!!!!! googletranslate
Thank you sir
Very nice presentation man. Really helpful
I am going to try this.
❤❤❤❤❤❤👍👍👍👍
Would building a housing around the propeller offer any advantages?
👌👌👌👌
at 14:34, BEFORE worrying about stabilizer Area, the SPAN of the horiz-stab should be Equal to THIRTY percent of wingspan.!!!!!! and, the Height of the vert-stab Should be a bit LESS-than Fifty percent, of THAT.!!!!!! googletranslate
at 18:18, the lower leading edge of the 'finished' profile/airfoil is less-than ideal.
at 16:15, the lower area of a rudder should NOT be removed.!!!!!!!!!!!!!!!!!!!!!!!!!!!!
consequently, when 33% is used in cg calculations,
the resultant answer is ALSO WRONG.!!!
at 7:31, it's FLATTTT not flate
at 11:32, you said 'times' not percent.
at 18:07, control horns are Not correctly configured.!!! at 18:13, WHY TF did you switch to a ZERO-dihedral wing.?!??!?!?! now, that kind of wing will HAVE to Have, ailerons.!!!!! googletranslate
at 17:38, this graphic is STILL WRONG.!!!!!! 33% is WRONG.!!!!!
it is MORE Precise to say that cg SHOULD be located at THIRTY percent of chord.!!!! or, if Desired, a BIT forward of thirty.!!!!! googletranslate
at 9:08, ailerons GO OUTBOARD.!!!!!! not inboard.!!!!!!!!!!
at 11:47, MORE WRONG STUFF.!!!!!!!!!!!! there is a REASON to correctly TAPER a tail boom. and, that tail boom AINT correctly tapered.!!!!!! i have details, if you want them. why does it say " 30 " , at the bottom line.???? yer system for 'measuring' fuselage length LESS-than ideal. specifically, the AFT End of the fuselage Should be considered to be at, the Elevator Trailing Edge.!!!!!!! googletranslate
at 8:55, servos do NOT go aft of the cg.!!!!!!! servos do NOT go aft of the cg.!!!!!!! servos do NOT go aft of the cg.!!!!!!! servos do NOT go aft of the cg.!!!!!!! googletranslate
at 7:02, you don't know what you are talking about. so, don't about stuff the you DON'T understand.