AN UNSTEADY TURBULENT BOUNDARY LAYER

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

[2] Johnson D.S., 1957, T ASME J APPL MECH, V24, P2

[3] KARLSSON SKF, 1958, THESIS J HOPKINS U

[4] KOVASZNAY LSG, 1948, SIMPLE ANAL CONSTANT

[5] KOVASZNAY LSG, 1958, SEMI ANN PROGR REP

[6] THE RESPONSE OF LAMINAR SKIN FRICTION AND HEAT TRANSFER TO FLUCTUATIONS IN THE STREAM VELOCITY [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1954, 224 (1156): : 1 - 23

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

[2] Johnson D.S., 1957, T ASME J APPL MECH, V24, P2

[3] KARLSSON SKF, 1958, THESIS J HOPKINS U

[4] KOVASZNAY LSG, 1948, SIMPLE ANAL CONSTANT

[5] KOVASZNAY LSG, 1958, SEMI ANN PROGR REP

[6] THE RESPONSE OF LAMINAR SKIN FRICTION AND HEAT TRANSFER TO FLUCTUATIONS IN THE STREAM VELOCITY [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1954, 224 (1156): : 1 - 23