Equations for Steady 1D Isentropic Flow

The equations used to describe steady 1D isentropic flow are derived from conservation of mass, momentum, and energy, as well as an equation of state (typically the ideal gas law). These equations are typically described as ratios between the local static properties (p, T, $latex \rho$) and their stagnation property as a function of Mach … Continue reading Equations for Steady 1D Isentropic Flow

Validation: Turbulent Zero Pressure Gradient Flat Plate – simpleFOAM, komegaSST

An excellent test case, and case to familiarize yourself with some of the turbulence models available in OpenFOAM is a 2D flat plate with zero pressure gradient. I will solve this problem using the solver simpleFoam and the komegaSST model. Here are the sections of this post: Quick Overview: kω-SST (komegaSST) Boundary Conditions Case set-up … Continue reading Validation: Turbulent Zero Pressure Gradient Flat Plate – simpleFOAM, komegaSST

Compressible Aerodynamics Calculator – Matlab

Here I have written a Matlab App for calculating compressible aerodynamics using the basic gas dynamics equations. The calculations available are: Isentropic Flow (including Prandtl-Meyer flow) Normal Shocks (See article) Oblique Shocks Fanno Flow Rayleigh Flow To install simply download the file from the Matlab File Exchange here: http://www.mathworks.com/matlabcentral/fileexchange/56152-compressiblecalccf?s_tid=srchtitle If you downloaded it prior to … Continue reading Compressible Aerodynamics Calculator – Matlab

Stationary Normal Shock Waves

Shock-waves are a common topic covered in undergraduate thermodynamics, fluid mechanics, and gas dynamics courses. Because shock-waves are awesome, I figured I would do one of my first posts on their basic theory. I'm going to try to cover the topic by first providing some context and a clear picture of what a shock wave … Continue reading Stationary Normal Shock Waves