Instrumentation for unsteady pressure measurement on cone cylinder configuration in NAL 1.2m Trisonic Wind 13; Tunnel

Srikantan, KV and Nirmala, GV (1988) Instrumentation for unsteady pressure measurement on cone cylinder configuration in NAL 1.2m Trisonic Wind 13; Tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    An instrumentation scheme adapted for' the measurement and analysis of unsteady pressure signals is detailed. Measurement scheme employed is useful for recording and analysis of unsteady pressures. Same can be extended for measurement of any unsteady signals.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Unsteady pressure measurement
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Poornima Narayana
    Date Deposited: 11 Aug 2006
    Last Modified: 24 May 2010 09:45
    URI: http://nal-ir.nal.res.in/id/eprint/2036

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