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0019070772
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Natural transition of boundary layers - The effect of turbulence, pressure gradient, and flow history
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A detailed investigation of the transitional boundary layer on the suction side of a turbine blade
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Campora, U.1
Pittaluga, F.2
Ubaldi, M.3
Zunino, P.4
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3
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0003692240
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Turbine blade entropy generation rate - Part I: The boundary layer defined
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ASME 2000-GT-265
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Davies, M.R.D., O'Donnell, F.K., Niven, A.J., "Turbine Blade Entropy Generation Rate - Part I: The Boundary Layer Defined", ASME 2000-GT-265.
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Davies, M.R.D.1
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4
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85040887359
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Loss mechanisms in turbomachines
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Denton, J.D.1
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7
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0028464779
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Effects of free stream turbulence and adverse pressure gradients on boundary layer transition
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Gostelow, J.P., Blunden, A.R., Walker, G.J., "Effects of Free Stream Turbulence and Adverse Pressure Gradients on Boundary Layer Transition", ASME, Vol. 116, July 1994.
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Gostelow, J.P.1
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8
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0036998214
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The effect of Reynolds number, compressibility and free stream turbulence on profile entropy generation rate
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Griffin, P.C.1
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9
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0023324597
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Influence of free stream turbulence and blade pressure gradient on boundary layer and loss behaviour of turbine cascades
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Hoheisel, H., Kiock, R., Lichtfuss, H.J., Fottner, L., "Influence of Free Stream Turbulence and Blade Pressure Gradient on Boundary Layer and Loss Behaviour of Turbine Cascades", ASME, Vol. 109, April 1987.
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Hoheisel, H.1
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Fottner, L.4
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10
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0024657477
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Aerodynamic design of low pressure turbines
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Boundary layers in turbomachines
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Mayle, R.E.1
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13
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85040295187
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Entropy production rates from viscous flow calculations, Part I - A turbulent boundary layer flow
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ASME 83-GT-70
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Moore, J., Moore, J.G., "Entropy Production Rates from Viscous Flow Calculations, Part I - A Turbulent Boundary Layer Flow", ASME 83-GT-70, 1983.
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Moore, J.1
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14
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0003692242
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Turbine blade entropy generation rate - Part II: The measured loss
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ASME 2000-GT-266
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O'Donnell, F.K. and Davies, M.R.D., "Turbine Blade Entropy Generation Rate - Part II: The Measured Loss", ASME 2000-GT-266.
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O'Donnell, F.K.1
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15
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84980163091
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Zur näherungsweisen Integration der Differentialgleichung der laminaren Reibungsschicht
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84885290207
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What should we measure?, An aeroengine turbine aerodynamic prospetive
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18
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0003510629
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Laminar boundary layers
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Investigation of aerodynamics and cooling of advanced engine turbine components:- Rotor blade aerodynamic design
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21
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84885290476
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Viscous flow theory - 1 laminar flow
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0002708231
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The use of transition region characteristics to improve the numerical simulation of heat transfer in bypass transitional flows
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Approximate calculation of the laminar boundary layer
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An approximate method for the calculation of the laminar and turbulent boundary layer by simple quadrature for two-dimensional and axially symmetric flow
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Numerical prediction of turbine profile loss
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