レイノルズ数がターボファンエンジンの飛行性能に及ぼす影響について

概要

論文の詳細を見る
The flight simulation test of F3-30 Iow bypass turbofan engine, which is installed on the next generation jet trainer for Japan Air Self Defense Force, was conducted at the AEDC of USAF, in order to get the flight performance data of this engine. As the test result it became clear that the Reynold's No. effects are very significant, especially for mass flow of fan and compressor, adiabatic efficiency of compressor and low pressure turbine and gas flow of low pressure turbine. The correlation factors for these parameters were found. Moreover the comparison for Wassell's method and also the comparison with the ATF-test data for engine performance were made and It was proven that the correlation factors were reasonable.
公益社団法人日本ガスタービン学会の論文
1988-12-10