Open AccessThe Motion of Strong Plane Shock Wave in Highly Viscous Medium
Author(s) -
Arvind Kumar,
AUTHOR_ID,
KAMLESH KUMAR,
AUTHOR_ID
Publication year - 2022
Publication title -
ultra scientist of physical sciences a
Language(s) - English
Resource type - Journals
eISSN - 2319-8044
pISSN - 2231-346X
DOI - 10.22147/jusps-a/340101
Subject(s) - adiabatic process , shock wave , mach number , shock (circulatory) , moving shock , plane (geometry) , mechanics , physics , overtaking , shock tube , mach wave , motion (physics) , classical mechanics , mathematics , thermodynamics , geometry , medicine , civil engineering , engineering
Neglecting the effect of overtaking disturbances, the motion of strong plane shock wave in highly viscous medium has been investigated by Chester-Chisnell- Whitham method. The analytical expressions for shock strength decreases as shock advances for low viscous region of a medium to the high viscous region. The dependence of mach number on propagation distance, Pressure and Particle velocity as well as on adiabatic index has also been analyzed for the cases. The results obtained here are also compared Yadav et al. (2008) for a freely propagating shock. The obtained expansions are computed and discussed through table.