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.