v^2(m*v)=thrust+drag(newton)/g

(r(x)rdx(m*v1=(m*v2)m/dt*vjet->1/2mv^2=-power(engine)+drag/(mgh)

denominator/numerator=fraction is part of a whole:

n+k/k-1=1

DEARS I BETTER RETREAT:

I HOPE THEY WORK IT OUT.

JAY LENO PLS:TXT

I’VE HEARD OF A SOLAR HEATED ROOM I’VE NEEVR HEARD OF A SOLAR HEATER

SO BASICALLY I LOVE GERMAN AND RUSSIAN PLANES…..

AND JAPANESE WITH A HINT OF PESTO TO BE VILE.

dears the rb52 ……..model-boeing no 7843#28B-U

a strato jets with f-119……..

basically gliders say teh following.

sin(m*g)=thrust/g=v:sink=cd

why why why why why whyw……….single bay biplanes…………

vs two bay biplanes!

four times the ernault thingy

or two times teh ernault thingy and ailerons……i call them spades like the royal airforce in britian.it’s very manouravreable……..it  a wide flip up wing.

miss hot memories:

sideview:78c=dyc(x)dx,topview:45+c=dy(x)dx/dz,

frontview:4+c=7(x)dy=3+4/c