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CFD Anderson.. Chapter 10: Supersonic Flow over a Flat plate |
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August 14, 2013, 10:34
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c code
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#21 | |
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Kerala
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August 21, 2013, 18:31
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#22 |
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shashi kumar
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can u send me a copy to me at karankumar9931034374@gmail.com
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October 17, 2013, 15:55
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M25 case for supersonic flow at 200,000ft
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#23 |
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sandy
Join Date: May 2013
Posts: 91
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Has anyone done the second case in Anderson CFD book ?
Mach=25 Alt=200,000ft (60km) L=0.005; I tried it and it gives me complex numbers. i used the free stream properties at that altitude. I used the same 70*70 grid . should i be missing something ? |
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February 11, 2015, 10:44
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Matlab code
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#24 |
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New Member
Join Date: Feb 2012
Posts: 14
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Hi,
I have uploaded a Matlab code that solves the original problem. It can be downloaded from MathWorks here: http://www.mathworks.com/matlabcentr...r-a-flat-plate Hope this helps! |
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July 11, 2020, 02:17
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C code
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#25 | |
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Srijit Sen
Join Date: Jul 2018
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