The paper covers the numerical simulation of the gas-dynamic parameters of the nozzle passage when using an intra-nozzle ramp interceptor in order to control the thrust vector. The analysis of the resulting axial and lateral forces at various angles of interceptor deflection is carried out.


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    Title :

    Investigation of Gas Flow Characteristics When Using Intra-Nozzle Interceptors to Control the Thrust Vector


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 65 , 4 ; 705-712


    Publication date :

    2022-10-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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