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AeroRocket
Software
specializes in high speed aerodynamics, Computational
Fluid Dynamics (CFD) and aerospace related software development for
rockets, airplanes and gliders. Other services include
wind tunnel
testing using AeroRocket's in-house built subsonic and supersonic
wind tunnels. |
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Preview
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Nozzle
is a one-dimensional compressible flow computer program
for the analysis of converging-diverging rocket nozzles. Nozzle
internal flow may be entirely subsonic, entirely supersonic or
a combination of subsonic and supersonic including shock waves
in the diverging part of the nozzle. Shock waves are clearly
identified as vertical red lines on all plots. The cross-sectional
shape in the axial direction of the nozzle is specified by selecting
from five standard nozzle types or by defining nozzle geometry
using the Free-Form nozzle geometry method. Nozzle plots color
contours of pressure ratio, temperature ratio, density ratio,
and Mach number and has a slider bar that displays real-time
values of all nozzle flow properties. New in this version is
the ability to determine shock-angle, jet-angle (plume-angle)
and Mach number for axisymmetric and two-dimensional nozzles
in the region near the lip for underexpanded and overexpanded
flow.
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