共 50 条
- [22] TURBULENT BOUNDARY-LAYER SHAPE AFTER A CORNER EXPANSION AERONAUTICAL JOURNAL, 1973, 77 (747): : 146 - 147
- [25] AN EXPERIMENTAL-STUDY OF THE COMPRESSOR ROTOR BLADE BOUNDARY-LAYER JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (02): : 364 - 373
- [27] EXPERIMENTAL-STUDY OF TURBULENT BOUNDARY-LAYER IN AXISYMMETRICAL CHANNELS IN PRESENCE OF DOWNSTREAM PRESSURE GRADIENT AND BLOW IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1977, (03): : 5 - 10
- [29] AN EXPERIMENTAL-STUDY OF THE INTERACTION OF AN UNSTEADY SHOCK WITH A TURBULENT BOUNDARY-LAYER AT MACH NUMBERS OF 1.3 AND 1.5 AERONAUTICAL JOURNAL, 1993, 97 (970): : 337 - 348
- [30] EXPERIMENTAL-STUDY OF THE 3-DIMENSIONAL TURBULENT BOUNDARY-LAYER IN FRONT OF A CYLINDER PERPENDICULAR ON A WALL FORSCHUNG IM INGENIEURWESEN-ENGINEERING RESEARCH, 1984, 50 (01): : 32 - 32