I received the TurboCAD stuff Friday (actually, I got it Saturday, but
it was delivered Friday :)). So I installed a copy, and started trying
it out. If you want a copy let me know, it is pretty good stuff.

Of course the best way to try out a CAD tool is to design something
useful with it. The something useful I tried was an aerospike engine:

http://lucifer.piratelabs.org/Rockets/spikelist.jpg
http://lucifer.piratelabs.org/Rockets/spikelist.TCW
http://lucifer.piratelabs.org/Rockets/spikelist.dxf

I have run into a few difficulties and learned quite a bit:

1. The actual location and size of the throat is not obvious. Twice I
dimensioned the spot where I thought the throat was to later find out
that there was a smaller area downstream of it. (The first time was just
a boneheaded DOH!, the second time was a subtle trick of conical
geometry.)

2. The throat dimension is going to be real tough to get right on the
scale we are working at. .020 inches is a ~400N thrust difference.

3. It looks like (from what little I have found) the "ramp" geometry is
fairly important to getting good performance and the proper flow fields.
The ramp on my drawing is pretty much wrong, I think. A NASA-AIAA paper
that I found uses a flow 28-34 deg off the center axis at the throat and
a cubic spline curve for the ramp. 

4. WOW!!! something is wrong with my calcs. I get theoretical numbers
from 3700N thrust and 132 Isp at 500m elavation (our test stand) up to
vacuum 5000N and 180 ISP. Okay, so vacuum performance is unattainable
even for an aerospike, but I am questioning my thermodynamic analysis -
does this seem reasonable for theoretical numbers at 300psi chamber
pressure and 85% HTP??

5. I really need to do some CFD on this. Does anyone know of a good
grid/mesh generation software package that is low-cost and easy to
obtain? I have some CFD code that should do exactly what I need
(AllSPD-3D from NASA Lewis) but generating a grid by hand is more tedium
than I can bear. 

Dave
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