A DIMENSIONLESS DESIGN FRAMEWORK AND MECHANISTIC STUDY OF A PERFORATED-WALL TRANSVERSE-JET MIXER FOR RAPID COOLING OF HIGH-TEMPERATURE GAS STREAMS
In conventional aero-engine testing, the combustor and afterburner are usually evaluated separately, which increases cost and energy consumption because two high-temperature sources are required. This study proposes a flange-type mixer for integrated testing, in which ambient air is transversely injected to cool the...