TURBINE FOR ORDNANCE TURBOJET ENGINEnⅡ - COLD-AIR PERFORMANCE WITH OPENED STATOR

摘要

A single-stage axial-flow turbine was investigated to determine the effect of increased stator throat area on the performance level of a turbojet engine turbine. The stator blades were bent to increase the throat area in order to move the compressor operating point in the engine farther away from surge. Results are compared with those obtained with the as-east stator setting.