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- [1] CALCULATION OF TEMPERATURE CONDITION OF TURBINE-BLADES WITH FILM COOLINGIZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1977, (03): : 132 - 135LOKAI, VIGUNCHENKO, EISHCHUKIN, AV
- [2] COOLING CHARACTERISTICS OF FILM-COOLED TURBINE-BLADESMECHANICAL ENGINEERING, 1984, 106 (06) : 86 - 86ABE, TDOI, NKAWAGUCHI, TYEMANE, TKUMAGI, TYOSHIDA, T
- [3] SOME FLOW PECULIARITIES AT FILM COOLING TURBINE-BLADESIZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1985, (03): : 96 - 98MILOVANOV, VK
- [4] FILM COOLING OF TURBINE-BLADES BY INJECTION FROM A ROW OF HOLESZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1988, 12 (03): : 159 - 172HAAS, WRODI, WSCHONUNG, B
- [5] EXPERIMENTAL INVESTIGATION RESULTS OF THE TEMPERATURE STATE OF TURBINE-BLADES WITH A PARTIAL-ROOT COOLINGIZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1983, (01): : 64 - 66ARKHIPOV, AIRUMYANTSEV, VVLIPATOV, NG
- [6] AERODYNAMIC LOSS PENALTY PRODUCED BY FILM COOLING TRANSONIC TURBINE-BLADESJOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1984, 106 (01): : 198 - 205HALLER, BRCAMUS, JJ
- [7] CONVECTIVE-FILM COOLING OF NOZZLE-TYPE TURBINE-BLADESHIGH TEMPERATURE, 1979, 17 (06) : 1095 - 1103ZIKEEV, VV
- [8] AERODYNAMIC LOSS PENALTY PRODUCED BY FILM COOLING TRANSONIC TURBINE-BLADESMECHANICAL ENGINEERING, 1983, 105 (06) : 88 - 88HALLER, BRCAMUS, JJ
- [9] EXIT LOSSES AT TURBINE-BLADES WITH POROUS COOLINGIZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1980, (03): : 46 - 49EPIFANOV, VMGUSKOV, VI
- [10] ON THE INFLUENCE OF THE VIBRATIONS OF A TURBINE DISK ON THE EIGENFREQUENCIES OF THE TURBINE-BLADESINGENIEUR ARCHIV, 1981, 50 (02): : 85 - 102IRRETIER, H