TURBULENT BOUNDARY-LAYER FLOW ON A ROTATING DISK

[1] BANKS WH, 1962, 27 NAT PHYS LAB SHIP

[2] Case P, 1966, J ROY AERO SOC, V71, P124

[3] CHAM TS, 1968, THESIS CAMBRIDGE U

[4] TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (02): : 91 - 108

[5] The flow due to a rotating disc. [J]. PROCEEDINGS OF THE CAMBRIDGE PHILOSOPHICAL SOCIETY, 1934, 30 : 365 - 375

[6] CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .2. ATTACHMENT-LINE FLOW ON AN INFINITE SWEPT WING [J]. AERONAUTICAL QUARTERLY, 1967, 18 : 150 - &

[7] CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .I. FLOW OVER REAR OF AN INFINITE SWEPT WING [J]. AERONAUTICAL QUARTERLY, 1967, 18 : 55 - &

[8] Dorfman L.A., 1963, HYDRODYNAMIC RESISTA

[9] Goldstein S, 1935, P CAMB PHILOS SOC, V31, P232

[10] ON THE STABILITY OF 3-DIMENSIONAL BOUNDARY LAYERS WITH APPLICATION TO THE FLOW DUE TO A ROTATING DISK [J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 248 (943) : 155 - 199

[1] BANKS WH, 1962, 27 NAT PHYS LAB SHIP

[2] Case P, 1966, J ROY AERO SOC, V71, P124

[3] CHAM TS, 1968, THESIS CAMBRIDGE U

[4] TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (02): : 91 - 108

[5] The flow due to a rotating disc. [J]. PROCEEDINGS OF THE CAMBRIDGE PHILOSOPHICAL SOCIETY, 1934, 30 : 365 - 375

[6] CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .2. ATTACHMENT-LINE FLOW ON AN INFINITE SWEPT WING [J]. AERONAUTICAL QUARTERLY, 1967, 18 : 150 - &

[7] CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .I. FLOW OVER REAR OF AN INFINITE SWEPT WING [J]. AERONAUTICAL QUARTERLY, 1967, 18 : 55 - &

[8] Dorfman L.A., 1963, HYDRODYNAMIC RESISTA

[9] Goldstein S, 1935, P CAMB PHILOS SOC, V31, P232

[10] ON THE STABILITY OF 3-DIMENSIONAL BOUNDARY LAYERS WITH APPLICATION TO THE FLOW DUE TO A ROTATING DISK [J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 248 (943) : 155 - 199