Design of transonic compressor research rig components

Sreenivasan, NR and Thunga, KS and Rameshaiah, MS (1972) Design of transonic compressor research rig components. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    This report outlines the details of the mechanical design of13; some of the components for the transonic compressor research rig. Details of design criterion and design data used for the rotor system as well as other components have been given. The final design chosen was very much influenced by the overall assembly limitations imposed and the compromise that had to be made in order to satisfy most of the requirements. A note on different designs envisaged during the course of the work has also been included with their relevant merits. Some of them could be used as an alternative design when testing rotors of different hub/tip ratios.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Rig components;Transonic compressor;Mechanical design;Rotor
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division, Propulsion Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 27 Nov 2006
    Last Modified: 24 May 2010 09:53

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