National Repository of Grey Literature 5 records found  Search took 0.01 seconds. 
Topical Problems of Fluid Mechanics 2016
Šimurda, David ; Bodnár, T.
The aim of the conference is to publish and to discuss the latest results of research in fluid mechanics.
Preliminary Study on Correlation between the Shape Parameter and the Skin Friction Coefficient in Transitional Zero Pressure Gradient Boundary Layer
Jonáš, Pavel
Paper is concerned with procedures to improve the accuracy of evaluations of the displacement thickness, the momentum thickness and the skin friction from measured mean velocity profiles, namely with regard to transitional boundary layers and to velocity profiles suffering from the lack of points in the immediate vicinity of the wall.
Evaluation of Interferograms of Unsteady Subsonic Airflow Past a Fluttering Airfoil
Šidlof, P. ; Riss, Š. ; Vlček, Václav
The paper reports on time-resolved interferometric measurements of unsteady ow elds around a uttering NACA0015 airfoil. A mechanical model with two degrees of freedom (pitch and plunge) has been designed and tested in a high-speed subsonic wind tunnel. Aeroelastic instability of the classical utter and dynamic stall type has been observed in the Mach number range M = 0.2 - 0.5. The interferograms were recorded using a Mach-Zehnder interferometer and a high-speed camera. An in-house software IFGPro was developed for the postprocessing and evaluation of the interferogram sequences, yielding pressure distribution, lift and drag force on the airfoil.
Modelling of the Laminar/Turbulenttransition on a Heated Flat Plate Using the k-kL-w Model
Kožíšek, Martin ; Fürst, J. ; Příhoda, Jaromír
The contribution deals with the numerical simulation of the transition to turbulence on a heated flat plate by means of the k-kL-k-kL-w model of Walters and Cokljat (2008). The revised version of the three-equation model was implemented into the OpenFOAM code for the incompressible and compressible flows. Numerical simulations of the boundary-layer development were carried out according to measurements of Sohn and Reshotko (1991). The transition model was tested by means of the skin friction and the Stanton number distributions for various free-stream turbulence levels. Results were compared with empirical correlations expressing the Reynolds analogy according to Kays and Crawford (1993) and with experimental data of Pinson and Wang (2000).
Simulation of Compressible Flow Through the Tip-Section Turbine Blade Cascade with the Unsteady Interaction of the Shock wave with Shear Layers
Straka, P. ; Příhoda, Jaromír ; Bobčík, M.
The contribution deals with the numerical simulation of compressible ow through the tip- section turbine blade cascade with the supersonic inlet boundary conditions. The simulation was carried out by the in-house numerical code using the explicit algebraic Reynolds stress model completed by the bypass transition model with the algebraic equation for the inter- mittency coefficient. The simulation was focused particularly on the shock-wave/boundary layer interaction resulting in combination of the bypass-transition and the separation induced transition.

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