Development of an Ejector for the ADA intake model static tests

Chidananda, MS and Venkatesh, S and Krishna Kumar, VS (1988) Development of an Ejector for the ADA intake model static tests. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    This report deals with the design and development" of An air-to-air ejector to facilitate testing of a 1/3 scale Aircraft intake model provided by ada . The objective was To develop an ejector having a mass augmentation ratio of About 8, with the primary air flow rate being 1 kg/s injecting At a pressure of about 0.66 mpa (gauge). A single stage, Single nozzle, constant area mixing type of ejector was developed for the purpose. This ejector had typical l/d ratio of about 7 and secondary to primary area ratio of about 60, producing a maximum augmentation ratio close to 7.5.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Ejector, Injector, GAS JET Booster, Mass Augmentor
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Advanced Composites Division, Propulsion Division
    Depositing User: Ms Indrani V
    Date Deposited: 24 Aug 2012 16:06
    Last Modified: 24 Aug 2012 16:06
    URI: http://nal-ir.nal.res.in/id/eprint/10850

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