Abstract
General attenuation laws for spherical shock waves were discussed in pure and dusty gases. The governing equations for the propagation of a spherical shock wave were solved numerically using the random choice method (RCM). It was shown that these laws helped in calculating the instantaneous primary shock wave Mach number to obtain the jump condition across it.
Original language | English |
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Pages (from-to) | 969-971 |
Number of pages | 3 |
Journal | AIAA Journal |
Volume | 39 |
Issue number | 5 |
DOIs | |
State | Published - 1 Jan 2001 |
ASJC Scopus subject areas
- Aerospace Engineering