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A laser tuft method was used to differentiate between boundary layer transition and separation on the suction surface of the blade.
On the OGV surface, boundary layer transition and separation affect the heat transfer significantly and they vary with the inlet flow angle.
To gain insight into boundary layer transition and separation for these low Reynolds number conditions, the heat transfer distribution on a Langston turbine blade shape was measured in a linear cascade wind tunnel for turbulence levels of 0.8%and10%0% and Reynolds numbers of 40 80k.
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Boundary layer transition estimation and modelling is essential for the design of many engineering products across many industries.
The data will be used to guide code developers by verifying their boundary layer transition models, and designers by showing the areas of the vane where heat transfer is most sensitive to the off-design conditions.
Such vehicle will have to be launched with a sounding rocket and shall re-enter the Earth atmosphere allowing to perform several experiments on critical re-entry technologies such as boundary-layer transition and shock shock interaction phenomena.
Boundary layer transition onset estimation and modelling are essential for the design of many engineering products across many industries.
Specifically in the cases in which the boundary layer transition plays an important role and the rotor performance are mostly influenced by transitional effects.
Laminar bubble, laminar separation and boundary layer transition are quite important phenomena that must be captured by the CFD model to reproduce the actual physical aerodynamic behavior.
The complex multiform flow phenomenon including boundary layer transition, lamination separation, turbulence attach line and re-lamination, boundary shock interaction and so on will appear when the air flow over the high lift configuration, which makes it very difficult to predict by numerical simulation.
In this paper, the Reynolds-averaged Navier Stokes are solved in conjunction with three additional transport equations to model and predict boundary layer transition.
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