sdubborn
robovane:isuzu damu
aerodynamics:couple about cg.
x/t=0,25*c*cl*s(profile)
x/t=sum(r,t)0,25*c*cl*s(wing)
x/t=-(sum(r,t)0,25*c*cl*s)+arm*thrust tail=0+drag(whole plane)
1/2m*v^2+m*g*h=equilibrium:n(nis even)*arm*sum(1,infinity)*forces/g
here goes nothing:
linearisation first,brackets,powers,squareroot,multiplication,division,addition,subtraction.
officer pls man…the judge will object…..
pitch=n*wrong/2*pi*diameter(propellor)
millenium.
lowcast….i b lowcast…….so low the clocks need retuning.
happy new year everybody…..
hosha hossannh.
i better close down the factory.
this will take a lot of prayers.
see that’s too weird.
terror in bed.
see i just averted the user.
juices and slime.