“…Over the past decades, numerous research efforts have been devoted to the investigation of resonant pulse combustors (RPC), including the groups of Roberts [1,2], Paxson [3,4], Gutmark [5][6][7], and Miller [8,9]. The primary objective of these efforts has been to enable a significant increase in gas turbine efficiency by replacing the constant pressure steady combustor found in conventional engines with a pulse resonant combustor.…”