Dutta, Vimala (1988) Application of Program Laws to LCA Planforms. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
This report presents the results of the computational work carried out for the lift analysis of LCA wings in supersonic flows using a computer software called LAWS [1]. The lifting pressure distribution and the associated force coefficients have been obtained for three planforms specified by the LCA group.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Wings;Supersonic flow |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Fluid Mechanics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 06 Aug 2012 11:25 |
| Last Modified: | 06 Aug 2012 11:25 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10675 |
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