Dutta, Vimala and Ramamoorthy, P (1988) Validation of a NASA code for determining the viscous supersonic flow past a pointed body of revolution. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
An existing NASA Code is validated on UNIVAC mining . the supersonic flow-past a pointed body 1100/71 for deterof revolution at zero incidence with a fully turbulent boundary layer. The programme geometry in any systerTi is suitably modified to allow the Input of body of units. Results for the test case of RM-10 body obtained by the NAL code and the original NASA code totally agree. Inviscid pressure13; by using this code are distributions on two bomb models obtained compared with those of Woodward's programme .
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Supersonic flow;Body of revolution |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Fluid Dynamics, Fluid Dynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 11 Aug 2006 |
| Last Modified: | 24 May 2010 09:45 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2023 |
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