CFD Analysis on Jet Decay Characteristics of Supersonic Jet through a CD Nozzle with a Cross-Wire
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Abstract
In this work, a computational fluid dynamics analysis is undertaken for establishing the decay characteristics through a CD nozzle fitted with a crosswire for a supersonic jet. The study focused on the axial jet decay and radial pressure distribution of unheated jets operating at Mach number 1.75 under various nozzle operating pressure conditions (NPR 5, 5.4 and 6.4). The results provide insights into the performance variance between the crosswire and baseline nozzles, particularly regarding flow characteristics, with implications for efficient nozzle design across diverse applications. Comparative analysis with experimental data revealed good agreement between the axial jet decay of the baseline nozzle and existing literature. Research on CD nozzle of circular jets with crosswire configurations at various operating conditions of over-expansion, near optimum and under-expansion conditions shows significant reductions in supersonic jet core length with the implication of crosswire, indicating enhanced mixing. Investigations into cross-wires with 2% blockage areas showed reductions in jet core length ranging from 10% to 29% compared to baseline nozzle jet.
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