共 50 条
- [21] AN EXPERIMENTAL-STUDY OF THE COMPRESSOR ROTOR BLADE BOUNDARY-LAYER [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (02): : 364 - 373
- [22] EXPERIMENTAL-STUDY OF AN INCIPIENT SPOT IN A TRANSITIONAL BOUNDARY-LAYER [J]. PHYSICS OF FLUIDS, 1982, 25 (10) : 1743 - 1751
- [23] EXPERIMENTAL-STUDY OF TURBULENT BOUNDARY-LAYER IN AXISYMMETRICAL CHANNELS IN PRESENCE OF DOWNSTREAM PRESSURE GRADIENT AND BLOW [J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1977, (03): : 5 - 10
- [25] AN EXPERIMENTAL-STUDY OF THE INTERACTION OF AN UNSTEADY SHOCK WITH A TURBULENT BOUNDARY-LAYER AT MACH NUMBERS OF 1.3 AND 1.5 [J]. AERONAUTICAL JOURNAL, 1993, 97 (970): : 337 - 348
- [26] EXPERIMENTAL-STUDY OF THE 3-DIMENSIONAL TURBULENT BOUNDARY-LAYER IN FRONT OF A CYLINDER PERPENDICULAR ON A WALL [J]. FORSCHUNG IM INGENIEURWESEN-ENGINEERING RESEARCH, 1984, 50 (01): : 32 - 32
- [29] TURBULENT-DIFFUSION IN EKMAN BOUNDARY-LAYER [J]. ATMOSPHERIC ENVIRONMENT, 1977, 11 (02) : 95 - 100
- [30] TURBULENT-DIFFUSION FROM A STATIONARY LINEAR SOURCE IN STRATIFIED ATMOSPHERIC SURFACE BOUNDARY-LAYER [J]. DOKLADI NA BOLGARSKATA AKADEMIYA NA NAUKITE, 1976, 29 (11): : 1609 - 1612