共 50 条
- [1] INFLUENCE OF MAINSTREAM TURBULENCE ON HEAT-TRANSFER COEFFICIENTS FROM A GAS-TURBINE BLADE JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 1994, 116 (04): : 896 - 903
- [2] Heat transfer in complex passages of turbine blade trailing edge Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2005, 31 (02): : 202 - 205
- [3] HEAT-TRANSFER AND TURBULENCE IN A TURBULATED BLADE COOLING CIRCUIT JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1994, 116 (01): : 169 - 177
- [5] TURBINE BLADE TRANSIENT HEAT-TRANSFER COMPUTER CODE JOURNAL OF AIRCRAFT, 1978, 15 (12): : 801 - 802
- [6] EXPERIMENTAL INVESTIGATION OF HEAT-TRANSFER ON TURBINE BLADE SURFACE IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1981, (01): : 37 - 41
- [7] SHORT DURATION MEASUREMENTS OF HEAT-TRANSFER RATE TO A GAS-TURBINE ROTOR BLADE JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1982, 104 (03): : 542 - 551
- [8] UNSTEADY APPROACH TO HEAT TRANSFER IN TURBINE BLADE COOLING PASSAGES. Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika), 1982, 25 (03): : 31 - 34
- [10] Heat-transfer measurements and predictions for the vane and blade of a (rotating high-pressure turbine stage JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 101 - 109