共 50 条
- [33] FILM COOLING ON A GAS-TURBINE BLADE NEAR THE END WALL [J]. MECHANICAL ENGINEERING, 1984, 106 (07): : 85 - 85
- [35] IMPROVEMENT OF GAS-TURBINE ENGINE PARAMETERS BY WATER INJECTION INTO TURBINE COOLING AIR [J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1983, (03): : 66 - 70
- [36] APPLICATION OF FILM COOLING THEORY TO COOLING OF AIRCRAFT GAS TURBINE CHAMBERS [J]. JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY, 1967, 71 (678): : 430 - &
- [37] EXPERIMENTAL INVESTIGATION OF FILM COOLING WITH EJECTION FROM A ROW OF HOLES FOR APPLICATION TO GAS-TURBINE BLADES [J]. JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1975, 97 (01): : 21 - 27
- [38] FILM COOLING OF GAS-TURBINE BLADES - STUDY OF EFFECT OF LARGE TEMPERATURE DIFFERENCES ON FILM COOLING EFFECTIVENESS [J]. JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1977, 99 (01): : 11 - 20
- [40] MHD GAS-TURBINE SYSTEMS DESIGNED FOR LOW COOLING WATER REQUIREMENTS [J]. JOURNAL OF ENERGY, 1983, 7 (06): : 542 - 548