Function mach_to_p_p0

pub fn mach_to_p_p0<F: Float>(mach: F, gamma: F) -> F

Total pressure ratio for given mach number and specific heat ratio

Examples

use comp_flow::mach_to_p_p0;

assert_eq!(mach_to_p_p0(0.0, 1.4), 1.0);
assert_eq!(mach_to_p_p0(1.0, 1.4), 0.5282817877171742);
assert_eq!(mach_to_p_p0(2.0, 1.4), 0.12780452546295096);