Alright lets do this.
Lets set up some fact to do our math by.
Temperature is constant for what i am doing. We all know its colder at 9000 feet, but for maths sake lets say its the same.
the equation for comparing gases is pv=nRt
P = the absolute pressure of the gas, in psi
n = number of moles, in lbmol
V = the volume of the gas, in ft3/lbmol
T = the absolute temperature of the gas absolute, in °R
R = the universal gas law constant of 10.7316 ft3·psi/(lbmol·°R)
we have 7.3L of air or 446 in^3.
Pressure is what we are changing
And everything on the right side is constant for what we are doing.
We will use a base of 446in^3 @ 14.7psi and compare all of our numbers to that.
446in^3 * 14.7psi = 6556.2
446in^3 * 10.46psi = 4665.16
again we see the 30% difference. Now in order to make up for the lost air we need to make 4.24lbs of boost. This is just right off the bat, right off idle you would have to make 4 lbs of boost to keep up.
Lets look at what happens when at sea level we are running at 14.7 lbs of boost.
446in^3 8 29.4psi = 13112.4
we have effectively doubled our displacement, back to 9000 ft.
in order to make the same amount of air we have to make almost 19psi of boost
446in^3 * (10.46psi + 18.94psi) = 13112.4
So it would seem you need to make about 4.25 extra lbs of boost than the rest of us at 9000 feet, all the time. So you are really looking to make boost somewhere in the range of 5psi to almost 23psi depending on how much equivalent boost you want to make.
I think this makes sense