I was wondering if anyone could post some formulas for me.

I had a general aerodynamics class in college years ago, and I've long since forgotten the lift formulas and drag formulas.

I remember there was one that you could calculate the lift a wing will produce given that you know the airspeed, temperature, air density (rho??), lift coefficient, and maybe angle of attack? (Cl may take care of this... like I said, it's been a long time)

I think there was another one where you could calculate the drag given the same parameters.

I remember we had a big table to look at to find rho at different conditions...

If anyone could post these formulas and maybe give me rho for a few different conditions, I'd be really thankful!

My elevation here is about 430 MSL, and if you could give me rho for Standard Atmosphere, 70F, 80, 90, and 100F, I'd really appreciate it!!

Or, if you could steer me to a website that would have the formulas, that would be great too!!

Thanks in advance!!