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- [21] PREDICTION OF GAS TURBINE ENGINE COMPRESSOR ROTOR BLADE SERVICE LIFE. Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1973, 16 (04): : 100 - 103
- [22] PROBABILISTIC MODELLING GEOMETRIC TOLERANCE AND LCF LIFE OF GAS TURBINE COMPRESSOR BLADE PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 10B, 2024,
- [23] 3-DIMENSIONAL APPROACH TO OPTIMIZATION OF A GAS-TURBINE DISK AND BLADE ATTACHMENT ASTRONAUTICS & AERONAUTICS, 1976, 14 (06): : B20 - B20
- [25] GAS-TURBINE COMPRESSOR INTERSTAGE COOLING USING METHANOL JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1983, 105 (04): : 859 - 864
- [27] A Comparative Thermoeconomic Study of Hybrid Solar Gas-Turbine Power Plants JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2014, 136 (01):
- [28] STUDIES IN INLET BRANCH PIPE OF GAS-TURBINE COMPRESSOR DOPOVIDI AKADEMII NAUK UKRAINSKOI RSR SERIYA A-FIZIKO-MATEMATICHNI TA TECHNICHNI NAUKI, 1977, (06): : 558 - 561