This paper proposes an engineering mathematical model for calculating and analyzing the triple configurations of propagating shock waves after a near-surface explosion. The developed model calculates and compares the parameters of blast waves and co-current flows behind them, characterizing the main damaging factors of an explosion, which is partially localized by a special device on board an aircraft.


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    Title :

    Calculation of the Loads behind the Triple Configuration of Partially Localized Shock Waves on the Aircraft Structural Elements


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 65 , 2 ; 311-318


    Publication date :

    2022-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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    ANDERSON, J. D. / MADDEN, M. T. | AIAA | 1971