Аннотация:http://icders2017.com/wp-content/uploads/26th_ICDERS_Program/Poster/26th%20ICDERS_submission_1104.pdf
This paper presents the results of numerical investigation of the process of propane-air mixture combustion in a rotating detonation wave enclosed in the space between two coaxial cylinders. The inlet flow conditions, including stagnation pressure and temperature, have been artificially set as slowly changing during detonation rotation, in order to catch the influence of these conditions on the process of rotation.