Desai, SS and Narayana, CL and Rangarajan, R (1985) Extension to the Panel Code NALSOP0509 to Include Design of Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
The code NALSOP0509, available in the SOFFTS Library of NAL has been extended to include a design of wing-body combinations to, minimize induced drag for specified lift and pitching moments at sub- or super--sonic flow conditions, Method of Lagrangean multiple is used to obtain the optimum camber and twist distributions for the wing in the presence of a body. SOFFTS Library of NAL has now been updated with this version of the code.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Wing design;Combat configurations;Drag optimization;Panel method |
| Subjects: | AERONAUTICS > Aerodynamics MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software |
| Division/Department: | Aerodynamics, Aerodynamics, Aerodynamics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 27 Sep 2012 14:40 |
| Last Modified: | 27 Sep 2012 14:40 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11030 |
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