ISSN No:2250-3676 ----- Crossref DOI Prefix: 10.64771
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Scholarly Peer Reviewed and Fully Referred Open Access Multidisciplinary Monthly Research Journal


    ANALYSIS OF AIR EJECTOR FLOW IN CONVERGENT AND CONVERGENT DIVERGENT NOZZLE OF AIRCRAFT

    ERRY SRIKANTH,BASINGALA PRAVEEN KUMAR

    Author

    ID: 1640

    DOI: Https://doi.org/10.64771/ijesat.2025.v25.i09.pp262-266

    Abstract :

    Ejectors Are Devices Often Used In Aircraft Systems. They Typically Have A Main Tube That Ends In A Nozzle, Which Is Usually Either Converging Or Converging-diverging In Shape. In This Study, We Focus On Improving How Well These Ejectors Work. The Main Goal Is To See If Changing The Nozzle From A Simple Converging Shape To A Converging-diverging Shape Can Make The Ejector More Efficient And Easier To Control. To Find Out, We Used Ansys Fluent Software To Analyze The Airflow Through The Ejector. We Looked At How Pressure, Temperature, And Speed Change Inside It. The Results Showed That Using A Convergingdiverging Nozzle Increases The Mass Flow Ratio, Which Means Better Performance, Compared To The Regular Converging Nozzle, All Based On The Same Size And Shape. Keywords: Nozzle, Ejector, Primary Flow, Secondary Flow, Mass Augmentation Ratio.

    Published:

    25-9-2025

    Issue:

    Vol. 25 No. 9 (2025)


    Page Nos:

    262-266


    Section:

    Articles

    License:

    This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

    How to Cite

    ERRY SRIKANTH,BASINGALA PRAVEEN KUMAR, ANALYSIS OF AIR EJECTOR FLOW IN CONVERGENT AND CONVERGENT DIVERGENT NOZZLE OF AIRCRAFT , 2025, International Journal of Engineering Sciences and Advanced Technology, 25(9), Page 262-266, ISSN No: 2250-3676.

    DOI: https://doi.org/10.64771/ijesat.2025.v25.i09.pp262-266