Narayana, CL (1986) Plotting routines for the panel code SOFO509. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A graphics code which can be used for viewing the13; geometric input to, or the output from, the panel code13; SOFO509 has been presented. The code also draws chordwise13; pressure coefficient and section load distributions along13; span. In all there are eight separate plots generated.13; Input to this code is from a file output from the panel code SOFO509. A Fortran listing of the code is given.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Wing-body combination;Plotting routines;Panelling;Section design;Pressure distribution;Section loads |
| Subjects: | MATHEMATICAL AND COMPUTER SCIENCES > Mathematical and Computer Scienes(General) |
| Division/Department: | Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 17 Aug 2006 |
| Last Modified: | 24 May 2010 09:47 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2375 |
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