Path: ACPro/ACEngine
% Compute the oblique shock angle from the streamline deflection angle.
Type ObliqueShockAngle for a demo showing oblique shock angles for a
range of Mach numbers.
--------------------------------------------------------------------------
Form:
theta = ObliqueShockAngle( m1, delta, gamma )
--------------------------------------------------------------------------
------
Inputs
------
m1 (1,1) Mach number after shock
delta (1,:) Streamline deflection angle
gamma (1,1) Fluid ratio of specific heats
-------
Outputs
-------
theta (1,:) Oblique shock angle
--------------------------------------------------------------------------
Reference: Ames Research Staff, "Equations, Tables and Charts for
Compressible Flow," Report 1135.
--------------------------------------------------------------------------
ACPro: ACEngine/MaxShockIncidenceAngle Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS
Back to the ACPro Module page