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- W1995459092 abstract "The thrust vectoring concept has been used for use in new advanced supersonic aircraft. This study presents the performance characteristics of the thrust vectoring nozzle by visualizing the shock behaviors with Schlieren method. The scaled models were designed and manufactured to see the shock behaviors of the various airflow condition. Also we executed experimental tests to see the geometrical effects of the thrust vector nozzle by changing pitch angle and length of pitch flaps. From this study we could understand the supersonic flow characteristics of the thrust vector nozzle. The total thrust of thrust vector nozzle is diminished by increasing the flap angle. But there is an optimum flap length ratio for attaining the highest thrust level and proper pitch effect." @default.
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- W1995459092 date "2011-09-30" @default.
- W1995459092 modified "2023-10-16" @default.
- W1995459092 title "Schlieren Visualization of the Thrust Vector Flowfield in a Supersonic Two-Dimensional Nozzle" @default.
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- W1995459092 doi "https://doi.org/10.5407/jksv.2011.9.3.030" @default.
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