detonations in oxygen-diluent mixtures are described for use in detonation studies.
Conditions addressed cover post-shock temperatures between 1300 and 2500K, pressures
between 1 and 100bar, and equivalence ratios from 0.5 to 2.0. These mechanisms were
developed through reduction from a detailed mechanism consisting of 193 reactions among
41 species that has been tested extensively against shock tube ignition times, counter flow …