Extension to the Panel Code NALSOP0509 to Include Design of Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment

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: Monograph (Project Report)
Uncontrolled Keywords: Wing design;Combat configurations;Drag optimization;Panel method
Subjects: AERONAUTICS > Aerodynamics
MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 27 Sep 2012 09:10
Last Modified: 27 Sep 2012 09:10
URI: http://nal-ir.nal.res.in/id/eprint/11030

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