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