hi
according to wikipedia (http://en.wikipedia.org/wiki/De_laval_nozzle):
A de Laval nozzle using hot air at a pressure of 1,000 psi (6.9 MPa or 68 atm), temperature of 1470 K, would have a pressure of 540 psi (3.7 MPa or 37 atm), temperature of 1269 K at the throat, and 15 psi (0.1 MPa or 1 atm), temperature of 502 K at the nozzle exit. The expansion ratio, nozzle cross sectional area at exit divided by area at throat, would be 6.8. The specific impulse would be 151 s (1480 N·s/kg).
as a result of the expansion of the exhust we see a drop in pressure from 37 atm to 1 atm, a drop of ~97.3%, to ~2.7% of the previous pressure , while the temperature will drom from 1269 K to 502 K a drop of ~60% to approximatly 40% of the previous pressure.
my question is rather straight forward, since this is an Adiabatic process, shouldn't the change in pressure be approximatly equal to the change in temperature? is there a way to calculate the ratio between the pressure drop and the temperature drop?