Additional details of the automatic data acquisition system attached to subsonic cascade tunnel

Manickam, MD (1987) Additional details of the automatic data acquisition system attached to subsonic cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The Subsonic Cascade Tunnel at NAL has been modified to13; carryout film cooling investigations under an ARDB project.13; Information on the facility and the vital components of the13; instrumentation system has been briefly outlined in an earlier report (Reference 1).13; Salient features of the Power Supply connections, Transducer connections. Stepper Motor Layouts. Multiplexer Chip connections and the AD 595 Chip connections of the Automatic Data Acquisition System (ADAS) attached to Subsonic Cascade Tunnel are given in this report.13; The information furnished can act as a reference file and13; will be usful in diagonising faults in case of malfunctioning of any of the systems.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Cascade Tunnel;Instrumentation
    Subjects: AERONAUTICS > Avionics & Aircraft Instrumentation
    Division/Department: Propulsion Division
    Depositing User: Deputy Head Poornima Narayana
    Date Deposited: 04 Aug 2006
    Last Modified: 24 May 2010 09:47
    URI: http://nal-ir.nal.res.in/id/eprint/2310

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