National Repository of Grey Literature 20 records found  1 - 10next  jump to record: Search took 0.00 seconds. 
Small Icing Wind Tunnel
Horák, V. ; Hoření, Bohumír ; Rozehnal, D. ; Svoboda, E.
The paper deals with a small icing wind tunnel realized at the Department of Aerospace and Rocket Technologies in conjunction with the aircraft icing simulation project. There are presented some results of the airfoil ice accretion prediction and various resulting ice shapes from icing wind tunnel. Appropriate consideration is given to the ice shape geometry measurement either.
Numerické řešení vzniku a narůstání námrazy
Hoření, Bohumír ; Horák, V. ; Chára, Zdeněk
Presented icing simulation is an aid to the certification process of small transport aircraft.
Project: Transition to turbulence modeling
Horák, V. ; Hoření, Bohumír
The project is focused on the transition from laminar to turbulent flow modelling. Developed code will be formulated in such a way to enable an effective parallel processing.
Numerické řešení nárůstu glazového ledu
Hoření, Bohumír ; Horák, V.
The paper presents the main problem of the wing airfoil glaze ice accretion prediction: theoretical solution of the flow of a thin layer on a cold surface and gradual freezing. There are formally arranged the conservative equations using for the solution of water flow in open channels. The flux terms are evaluated using a discontinuous Galerkin method, which could be considered as a generalized finite volumes classical method.
Numerické simulace a experimentální měření pulzačního proudění
Chára, Zdeněk ; Hoření, Bohumír
The contribution presents numerical as well as experimental investigations of laminar and turbulent pulsating flow in an initial part of a rigid pipe. The simulations were performed with help of Fluent 6.3. Measurements of velocity profiles were done by an ultrasound velocity monitor UVP.
Geometrická a funkcionální diskretizace vyšších řádů pro Navier-Stokosovy rovnice
Hoření, Bohumír ; Chára, Zdeněk
The paper deals with an applicability of high order methods for geometrical as well as functional approximations. Usefulness of this approach is demonstrated on selected examples.
Shear-driven cavity flow at high Reynolds numbers
Chára, Zdeněk ; Kysela, Bohuš ; Hoření, Bohumír
The paper deals with a research of a shear-driven cavity flow at high Reynolds numbers (Re= 12000-100000). PIV method was used with a continuous light source and at selected profiles LDA method was used, too. Numerical k-omega, SST model was used for the same range of the Reynolds numbers.
Modelování klasické námrazy na profilu křídla
Horák, V. ; Hoření, Bohumír
The paper presents the rime ice accretion prediction code. Model includes the calculation of a velocity distribution, droplet motion equations and detetrmination of a water mass flux impacting on the wing airfoil surface. Changing the airfoil shape is illustrated in compare of experimental results.
Lokální odpory na stěně umístěných překážek
Chára, Zdeněk ; Hoření, Bohumír
The influence of surface mounted obstacles on free level of channel flow is discussed. The obstacles of square cross section are placed sequentially along a hydraulic flume and perpendicularly to the flow direction across the whole channel width. Three various spacing between the obstacles - 5H, 11H and 23H (H is height of the obstacle) were tested for different flow discharges. The surface levels were recorded and the results were compared with numerical simulations. Based on the experimental data and numerical simulations the resistance coefficients of the individual obstacles were determined.
Numerical simulation of flow in a backward step channel
Hoření, Bohumír ; Chára, Zdeněk
The contribution deals with numerical simulations of flow in a backward step channel of step height 2 cm and channel cross section 2x20 cm. The simulations are performed with help of three turbulent models – k-w SST, standard k-e and Reynolds Stress Model on three different types of grid. The results are compared with experimental observation. The best results were achieved for k-w SST model.

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