共 50 条
- [1] FILM COOLING ON A GAS-TURBINE ROTOR BLADE [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1992, 114 (04): : 828 - 834
- [2] FILM COOLING ON A GAS-TURBINE BLADE NEAR THE END WALL [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (01): : 117 - 122
- [3] FILM COOLING ON A GAS-TURBINE BLADE NEAR THE END WALL [J]. MECHANICAL ENGINEERING, 1984, 106 (07): : 85 - 85
- [4] MIXED CONVECTION THERMOSYPHON, AND GAS-TURBINE BLADE COOLING [J]. MECHANICAL ENGINEERING, 1974, 96 (04): : 81 - 81
- [5] EVALUATION TECHNIQUE OF GAS-TURBINE BLADE COOLING SYSTEM EFFICIENCY [J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1991, (04): : 27 - 30
- [7] ANALYSIS OF FILM COOLING AND FULL COVERAGE FILM COOLING OF GAS-TURBINE BLADES [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1984, 106 (01): : 206 - 213
- [9] AERODYNAMIC LOSS IN A GAS-TURBINE STAGE WITH FILM COOLING [J]. JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1980, 102 (04): : 964 - 970
- [10] Constructal entransy dissipation rate minimization for gas-turbine blade cooling [J]. Chen, L. (lgchenna@yahoo.com), 1600, Chinese Mechanical Engineering Society (50): : 142 - 149