| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5374423 | Chemical Physics | 2012 | 7 Pages |
Abstract
⺠We evaluate the vibrational non-equilibrium in oxygen hypersonic boundary layer flows. ⺠We adopt a state-to-state vibrational kinetics model. ⺠We use updated quasicassical trajectory atom-molecule collision rate coefficients. ⺠Multiquanta transitions and direct dissociation-recombination are important. ⺠We calculate the heat flux through the boundary layer.
Related Topics
Physical Sciences and Engineering
Chemistry
Physical and Theoretical Chemistry
Authors
I. Armenise, F. Esposito,