Compute relative pressure ratio
d = rrdelta(p0, mach, g)
d = rrdelta(p0, mach, g)
computes m
pressure
relative ratios, d
, from m
static
pressures, p0
, m
Mach numbers, mach
,
and m
specific heat ratios, g
. p0
must
be in pascals.
Determine the relative pressure ratio for three pressures:
delta = rrdelta([101325 22632.0672 4328.1393], 0.5, 1.4) delta = 1.1862 0.2650 0.0507
Determine the relative pressure ratio for three pressures and three different heat ratios:
delta = rrdelta([101325 22632.0672 4328.1393], 0.5, [1.4 1.35 1.4]) delta = 1.1862 0.2635 0.0507
Determine the relative pressure ratio for three pressures at three different conditions:
delta = rrdelta([101325 22632.0672 4328.1393], [0.5 1 2], [1.4 1.35 1.4]) delta = 1.1862 0.4161 0.3342
For cases in which total pressure ratio is desired (Mach number is nonzero), the total pressures are calculated assuming perfect gas (with constant molecular weight, constant pressure specific heat, and constant specific heat ratio) and dry air.
Aeronautical Vestpocket Handbook, United Technologies Pratt & Whitney, August, 1986