rrdelta
Compute relative pressure ratio
Syntax
Description
Examples
Input Arguments
Output Arguments
Limitations
For cases in which total pressure ratio is desired, that is, the Mach number is nonzero, the function assumes perfect gas — with constant molecular weight, constant pressure specific heat, and constant specific heat ratio — and dry air when calculating total pressures.
References
[1] Pratt & Whitney Aircraft. Aeronautical Vestpocket Handbook. United Technologies, August 1986.
Version History
Introduced in R2006b