mach_number_comp.py

class openconcept.analysis.atmospherics.mach_number_comp.MachNumberComp(**kwargs)

Bases: openmdao.core.explicitcomponent.ExplicitComponent

This component computes Mach number from stagnation Mach number, density, speed of sound, and pressure.

Adapted from: J.P. Jasa, J.T. Hwang, and J.R.R.A. Martins: Design and Trajectory Optimization of a Morphing Wing Aircraft 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference; AIAA SciTech Forum, January 2018