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7 ___________________________________________________
 
 
 
UDC 629.764:25+577.7
 
Technical mechanics, 2018, 1, 72 - 83 
SIMULATION OF THE EVOLUTION OF A DROPLET CLOUD THROWN INTO THE ATMOSPHERE AS A RESULT
 OF AN EXPLOSION OF A LAUNCH VEHI-CLE WITH SELF-INFLAMMABLE PROPELLANT COMPONENTS
 
DOI:
https://doi.org/10.15407/itm2018.01.072
 
 
Gorbuntsov V. V., Zavoloka O. M., Kremena A. P., Svyrydenko M. F. 
 
Gorbuntsov V. V.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
 Ukraine
 
 Zavoloka O. M.
 Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
 Ukraine
 
 Kremena A. P.
 Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
 Ukraine
 
 Svyrydenko M. F.
 Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
 Ukraine
 
 
      
The aim of this work is to develop a methodological approach to simulating the evolution
 of a droplet cloud (DC) formed as a result of an explosion of a launch vehicle with
 self-inflammable propellant components in the initial portion of the flight trajectory
 and thrown into the atmosphere with initial motion parameters that correspond to the
 launch vehicle position at the time of the explosion. The proposed approach, which
 is based on a phenomenol-ogical analogy with the motion of a fuel spray injected
 in the combustion chamber of a diesel, takes into account the fragmentation and tracing
 of droplets and the effect of their collisions and possible coalescence on the structure
 and parameters of the propellant component DC, which undergoes a transformation as it moves.
 The proposed model of the DC evolution, which is due to droplet interaction in the DC and its
 structuring in the process of mo-tion, reflects the most important, in terms of the environmental
 consequences of the explosion, processes in the DC and allows one to estimate its basic kinematic
 and geometric characteristics required for solving the ballistic prob-lem of the motion of the
 suspended DC droplets in the atmosphere and their precipitation onto the ground surface.
                   
 
 
 
 explosion, droplet cloud, droplet, propellant component, launch vehicle
 
                   
 
 
 
 
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DOI:
https://doi.org/10.15407/itm2018.01.072
 
 
Copyright (©) 2018 Gorbuntsov V. V., Zavoloka O. M., Kremena A. P., Svyrydenko M. F. 
 
Copyright © 2014-2018 Technical mechanics
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