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.
Calculation of the Loads behind the Triple Configuration of Partially Localized Shock Waves on the Aircraft Structural Elements
Russ. Aeronaut.
Russian Aeronautics ; 65 , 2 ; 311-318
2022-04-01
8 pages
Article (Journal)
Electronic Resource
English
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