Three-dimensional inverse method for turbomachinery blading design
A Demeulenaere, R Van den Braembussche - 1998 - asmedigitalcollection.asme.org
An iterative procedure for three-dimensional blade design is presented, in which the three-
dimensional blade shape is modified using a physical algorithm, based on the transpiration
model. The transpiration flux is computed by means of a modified Euler solver, in which the
target pressure distribution is imposed along the blade surfaces. Only a small number of
modifications is needed to obtain the final geometry. The method is based on a high-
resolution three-dimensional Euler solver. An upwind biased evaluation of the advective …
dimensional blade shape is modified using a physical algorithm, based on the transpiration
model. The transpiration flux is computed by means of a modified Euler solver, in which the
target pressure distribution is imposed along the blade surfaces. Only a small number of
modifications is needed to obtain the final geometry. The method is based on a high-
resolution three-dimensional Euler solver. An upwind biased evaluation of the advective …
[图书][B] Three-dimensional inverse method for turbomachinery blading design
A Demeulenaere, R Van den Braembussche - 1996 - asmedigitalcollection.asme.org
An iterative procedure for 3D blade design is presented. The three-dimensional blade shape
is modified using a physical algorithm, based on the transpiration model. The transpiration
flux is computed by means of a modified Euler solver, in which the target pressure
distribution is imposed along the blade surfaces. Only a small number of modifications is
needed to obtain the final geometry. The method is based on a high resolution three-
dimensional Euler solver. An upwind biased evaluation of the advective fluxes allows for a …
is modified using a physical algorithm, based on the transpiration model. The transpiration
flux is computed by means of a modified Euler solver, in which the target pressure
distribution is imposed along the blade surfaces. Only a small number of modifications is
needed to obtain the final geometry. The method is based on a high resolution three-
dimensional Euler solver. An upwind biased evaluation of the advective fluxes allows for a …
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