Відео

🎉🎉🎉🎉🎉nice👍

Fly nhi hua kua

WowwwwEeeee🎉🎉🎉🎉🎉

🩷🩷💞💞🩷🩷

Standard ka use Karo yeh sab toh duplicate maal

🎉☺️💥👍🎇🎆🧨🪅🪔

❤❤❤❤❤❤🎉🎉🎉🎉❤❤❤🎉🎉🎉😊😊😊

👍❤❤❤❤❤❤👌

❤❤❤❤🎉🎉

❤❤❤❤❤❤❤🎉

Xxx

plan link sir

Jay Shri Ram Jay Shri Ram ❤❤❤❤❤❤❤❤ 0:17

Happy Vijay Dashami जय श्रीराम 🙏🏻🕉

एक नम्बर❤❤🎉🎉

❤❤❤❤❤❤

You are so talented god bless you and good luck for your next video 👍

Very nice keep it up 👏

Very good 👍

Super duper excited for next video ❤❤

Chha gaye bhaiya.ek number ❤❤

Good bro

Very nice bro

🎉WOW🎉

Good bro❤❤

3356 aileron control horns have NOT been correctly installed. 3608 main landing gear not correctly located.

2040 servos do NOT go at the tail.! 3121 the main spar goes at THIRTY PERCENT of chord. the main spar should be Contiguous and should SPAN the width of the fuselage.! 3200 the design of a dihedral wing should include a CENTER section and dihedral BRACE. 3308 aileron servos should be located forward-of thirty percent of chord and as far inboard as is practical.

0544 where a pusher thrust system is used, THE PARTS of the model located in front of the prop BLOCK air flow to the prop.! design of the fuselage should, therefore, be INFORMED by this fact.!

0057 the trailing edge of a rudder should be a single straight line; that is parallel to the hinge line.!!! ideally, the rudder hinge line should be Perpendicular to the center line (of the aircraft). the tips of the horiz-stab should be PARALLEL to the air flow.! the main landing gear should be located below the cg. the cg should be located at THIRTY percent of chord.! if/when, as here, the tail is Heavy, the cg may need to be located forward-of thirty percent. (thirty percent is a Multiplication by .3.) at the nose, the relatively uninterrupted upper surface is going to make unscheduled negative lift/downforce. googletranslate

an aircraft that has a propulsion system is NOT a glider.!

0015 servos do NOT go at the tail.!!!!!! ailerons and elevator Should Extend to the wingtips/stab tips. 0026 the nose SHOULD be tapered/contoured in BOTH axes.!!! it is not recommended that the rudder/elevator be Directly in the prop wash.! googletranslate

🎉🎉🎉🎉🎉🎉

Very nice

Wow wonderful 🎉😊

excellent nice finishing

115 the internal structure of the building material should be Correctly oriented. was NOT done here. 120 the lines (by blue pin) SHOULD be PARALLEL to the air flow.! if they are not, angled surfaces make More Drag.! 510 there is no reason to use two cable ties when ONE will do the job.! instead, a couple drops of glue WOULD hold those components in place.! same with servos.! 739 it should be understood that tailerons provide incomplete control. 753 FILLING a hole with glue should be avoided.! bc doing so results in an avoidable increase in the all-up-weight (auw) and contributes to a less-than optimal dom. distribution of mass. the use of a two engine reference design is NOT recommended. bc doing so results in a 'bulkier' tubular structure. such a fuselage structure makes relatively More Drag and causes more obstruction of air flow to the prop.! googletranslate

www.youtube.com/@Krexperiment17