共 50 条
- [32] DESIGN REVIEW OF CERAMIC COMPONENTS FOR TURBINE ENGINES. Journal of Engineering for Power, Transactions ASME, 1980, 102 (02): : 437 - 447
- [33] Regarding the similarity of compressible fluid turbine engines. COMPTES RENDUS HEBDOMADAIRES DES SEANCES DE L ACADEMIE DES SCIENCES, 1941, 213 : 682 - 685
- [34] Damageability of Turbine Disk Material in Stress Concentration Zones After Long Operation in Gas Turbine Engines. Problemy Prochnosti, 1980, (11):
- [35] Problems of Shell Calculations for Aircraft Turbine Engines. Mechanika Teoretyczna i Stosowana, 1980, 18 (03): : 391 - 399
- [36] Topology optimization design method on compressor disks in gas turbine engines Tuijin Jishu/Journal of Propulsion Technology, 2014, 35 (06): : 830 - 837
- [37] SOLUTION OF THE INVERSE PROBLEM OF DETERMINING THE THERMODYNAMIC PROPERTIES OF THE WORKING FLUID OF GAS TURBINE ENGINES. Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1984, 27 (02): : 124 - 125
- [39] Experience of Application of Holographic Interferometry to Investigate Vibration of Rotor Elements of Gas Turbine Engines. Problemy Prochnosti, 1976, (05): : 85 - 87
- [40] COMPARATIVE ANALYSIS OF THE BASIC COMBUSTION CHARACTERISTICS OF SOME HEAVY HYDROCARBON FUELS IN APPLICATION TO AIRCRAFT GAS TURBINE ENGINES. Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1979, 22 (03): : 51 - 55