Experimental and computational simulation of in-flight icing phenomena
RJ Kind, MG Potapczuk, A Feo, C Golia… - Progress in Aerospace …, 1998 - Elsevier
This paper reviews experimental and computational methods used for simulation of ice
accretion on aircraft flying through icing conditions. Such methods were recently reviewed …
accretion on aircraft flying through icing conditions. Such methods were recently reviewed …
[图书][B] Convective heat and mass transfer
WM Kays, ME Crawford, B Weigand - 1980 - academia.edu
Some of the problems in the text are brief exercises leading to single numerical or algebraic
results, but the great majority are much more extensive investigations, some approaching …
results, but the great majority are much more extensive investigations, some approaching …
The influence of large-scale high-intensity turbulence on vane heat transfer
FE Ames - 1997 - asmedigitalcollection.asme.org
An experimental research program was undertaken to examine the influence of large-scale
high-intensity turbulence on vane heat transfer. The experiment was conducted in a four …
high-intensity turbulence on vane heat transfer. The experiment was conducted in a four …
[图书][B] Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade
VK Garg, AA Ameri - 2001 - asmedigitalcollection.asme.org
Two versions of the two-equation k-ω model and a shear stress transport (SST) model are
used in a three-dimensional, multi-block, Navier-Stokes code to compare the detailed heat …
used in a three-dimensional, multi-block, Navier-Stokes code to compare the detailed heat …
The transient liquid crystal technique: Influence of surface curvature and finite wall thickness
G Wagner, M Kotulla, P Ott, B Weigand… - J …, 2005 - asmedigitalcollection.asme.org
The transient liquid crystal technique is currently widely used for measuring the heat transfer
characteristics in gas turbine applications. Usually, the assumption is made that the wall of …
characteristics in gas turbine applications. Usually, the assumption is made that the wall of …
Heat transfer research on gas turbine airfoils at NASA GRC
VK Garg - International Journal of Heat and Fluid Flow, 2002 - Elsevier
The turbine gas path is a very complex flow field due to a variety of flow and heat transfer
phenomena encountered in turbine passages. This manuscript provides an overview of the …
phenomena encountered in turbine passages. This manuscript provides an overview of the …
The effect of turbulence intensity and length scale on low-pressure turbine blade aerodynamics
RJ Butler, AR Byerley, K VanTreuren… - International journal of …, 2001 - Elsevier
Unpredicted losses have been observed in low-pressure gas turbine stages during high
altitude operation. These losses have been attributed to aerodynamic separation on the …
altitude operation. These losses have been attributed to aerodynamic separation on the …
The effects of freestream turbulence, turbulence length scale, and exit Reynolds number on turbine blade heat transfer in a transonic cascade
This paper experimentally investigates the effect of high freestream turbulence intensity,
turbulence length scale, and exit Reynolds number on the surface heat transfer distribution …
turbulence length scale, and exit Reynolds number on the surface heat transfer distribution …
[图书][B] Blade heat transfer measurements and predictions in a transonic turbine cascade
PW Giel, GJ Van Fossen, RJ Boyle, DR Thurman… - 1999 - asmedigitalcollection.asme.org
Detailed heat transfer measurementa and predictions are given for a turbine rotor with 136°
of turning and an axial chord of 12.7 cm. Data were obtained for inlet Reynolds numbers of …
of turning and an axial chord of 12.7 cm. Data were obtained for inlet Reynolds numbers of …
Experimental measurements and modeling of the effects of large-scale freestream turbulence on heat transfer
The influence of freestream turbulence representative of the flow downstream of a modern
gas turbine combustor and first stage vane on turbine blade heat transfer has been …
gas turbine combustor and first stage vane on turbine blade heat transfer has been …