Some design considerations for a transient load protection system for aeroelastic testing of rocket models in the NAL blowdown tunnel.

Suryanarayana, BG (1974) Some design considerations for a transient load protection system for aeroelastic testing of rocket models in the NAL blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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    Abstract

    Aeroelastic evalustion of satelite launch whiich configurations is to be undertaken at NAL under a contmet from VSSC(ISDO) an aeronautically cumulated 1/45th scale SLV-3 model is to be tested in the NAL 1'X 1' trisonic blowdown tunnel. such an aeroelastic model is generally too fragile to withatand the transient aerodynamic lodds occuring at the tunnel starting and stopping. An effective mears of protecting the model against such loads is needed.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: National Trisonic Aerodynamic Facility
    Depositing User: Poornima Narayana
    Date Deposited: 31 Aug 2006
    Last Modified: 24 May 2010 09:49
    URI: http://nal-ir.nal.res.in/id/eprint/2532

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