IGTC-102 Application of Advanced Technology to Modern Military Turbofan Engines(Organized Session I IMPROVEMENTS OF GAS TURBINE ENGINES IN AIRCRAFT APPLICATIONS)
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概要
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The combat aircraft requirement is for high thrust/weight ratio in combat, but low fuel consumption while patrolling to minimise aircraft size. This is achieved with high flame temperatures, medium bypass ratio, high overall pressure ratio and of course good component efficiencies. This paper concerns itself with the interaction of design and manufacturing technology in achieving high engine and component efficiency which demands 3D aerodynamic design and manufacturing capability with high precision.
- 公益社団法人日本ガスタービン学会の論文