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