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