共 2 条
- [1] SIMPLIFIED TREATMENT OF THE TURBULENT BOUNDARY LAYER ALONG A CYLINDER IN COMPRESSIBLE FLOW [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (01): : 23 - &
- [2] SKIN-FRICTION AND HEAT-TRANSFER CHARACTERISTICS OF A LAMINAR BOUNDARY LAYER ON A CYLINDER IN AXIAL INCOMPRESSIBLE FLOW [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (10): : 671 - 675