Shock wave propagation through air: a reactive molecular dynamics study

Abstract

Shock compression of air is observed in numerous situations ranging from explosions to hypersonic vehicle entry into atmosphere. In an effort to develop continuum-based equation of state for air subjected to shock compression, it is necessary to understand the dynamics of the shock compression process with regards to formation of new chemical species in air at the molecular level. With this in perspective, three different models of air (consisting a mixture of O 2 , N 2 and CO 2 gas, with or without H 2 O based on presence of humidity) are subjected to shock compression ranging from 0.5 km s −1 to 5.0 km s −1 particle velocities. Thermodynamic quantities are evaluated to plot Rankine Hugoniot planes for the three different air models: dry air at mean sea level (MSL), humid air at MSL and dry air at high altitude level of 36 000 ft above MSL. It is observed that high shock velocities eventually results in dissociation of gaseous molecules and formation of new gaseous species which has been quantified in the manuscript.

Document Details

Document Type
Pub Defense Publication
Publication Date
Mar 01, 2021
Source ID
10.1098/rspa.2020.0676

Entities

People

  • Ritwik Ghoshal
  • Subhadeep Pal

Organizations

  • Indian Institute of Technology Kharagpur
  • Office of Naval Research Global

Tags

Readers

  • Atmospheric Science/Meteorology
  • Combustion Dynamics and Shock Wave Physics.
  • Computational Fluid Dynamics (CFD)

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow