Application-of experimental and theoretical methods for13; prediction of steady and unsteady loads on flexible swept, tapered and delta wings: PALAST-1

Ramamurthy, MR and Rajagopal, P (1991) Application-of experimental and theoretical methods for13; prediction of steady and unsteady loads on flexible swept, tapered and delta wings: PALAST-1. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The proposed programme broadly aims to explore the possibilty of formulating important design guidelines/ tools pertaining to the prescription of the aerodynamic design load from aeroealstic considerations and thereby aims to bring the aeroelasticity concepts closer to the aerospace structural design cycle .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aeroelasticity;Aerodynamic loads;Design tools
    Subjects: MATHEMATICAL AND COMPUTER SCIENCES > Mathematical and Computer Scienes(General)
    Division/Department: Structures Division, Structures Division
    Depositing User: Mr. N A
    Date Deposited: 24 Jun 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1780

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