Performance evaluation of a cold-air turning

Murugesan, K and Sankaranarayanan, S and Ramasastry, S (1975) Performance evaluation of a cold-air turning. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Cold Air investigation of a single stage axial turbine13; designed and fabricated at N.A.L., was carried out over a wide range of operating conditions. Using the experimental values obtained, the non dimensional parameters of the turbine were Calculated and the performance graphs were drawn. The estimated values of power and efficiency were compared with the corresponding experimental values at the design conditions. At the design pressure ratio, the13; best operating condition was suggested to get maximum specific power.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Cold air;Axial turbine;Pressure ratio
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Propulsion Division, Propulsion Division, Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 10 Nov 2006
    Last Modified: 10 Sep 2015 14:01

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