Generated lift is equal to the lift coefficient (Cl) times the density of the air (r) times half of the square of the velocity (V) times the WING AREA (A).
Now some come here with willingness to learn, others not so much. Chose whatever path you want, but cutting and quoting posts out of context is certainly a valid way to go, if that is the choice you've made. Also, did you fail to notice that "at airshow speeds that the OP mentions" disclaimer i put in that post? Or was it convenient to omit it? It's in your quote after all.