Experimental data describing laminar separation bubbles developing under strong adverse pressure gradients, typical of ultra-high-lift turbine blades, have been analyzed to define empirical correlations able to predict the main features of the separated flow transition. Tests have been performed for three different Reynolds numbers and three...
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2019 (v1)PublicationUploaded on: April 14, 2023
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2019 (v1)Publication
An experimental data base on attached and separated-flow transitional boundary layers, under various levels of free-stream turbulence, Reynolds number and pressure gradient has been composed, with the aim of providing high-accuracy data and boundary conditions for development and testing of laminar-to-turbulent transition models. Experiments...
Uploaded on: April 14, 2023