National Repository of Grey Literature 28 records found  beginprevious19 - 28  jump to record: Search took 0.01 seconds. 
Řízení přechodu a odtržení mezní vrstvy na profilech a tělesech za podmínek volné atmosféry
Popelka, Lukáš ; Zelený, L.
The paper deals with visualisation of uncontrolled and controlled cases of boundary layer transition and separation carried out during in-flight measurements. Oil flow and tuft techniques have been applied. Influence of passive flow control devices to the performance of the entire aircraft has been established and importance of active and adaptive approach shown.
O stopách turbulence v průběhu zkráceného přechodu mezní vrstvy
Jonáš, Pavel ; Elsner, W. ; Mazur, Oton ; Uruba, Václav ; Wysocki, M.
The wall-friction records made in the transitional region of boundary layer were analysed using Narasimha's transitional intermittency concept and wavelet analysis. The distributions of the dimensionless spot production rates clarify the effect of outer stream turbulence structure on the course of laminar/turbulent boundary layer transition.
O stopě turbulence a tišině
Jonáš, Pavel
The purpose of the contribution is to collect information on the generation, propagation and coalescence of turbulent spots and calmed regions in a transitional boundary layer. The appreciation of the behaviour of both turbulent spot and calmed region under turbulent free stream is the focus of this study.
Experimentální a numerické vyšetřování nestacionárního chování impaktního proudu do korýtkové kavity
Knob, Martin ; Antoš, Pavel ; Adamec, J.
In this contribution, the unsteady behaviour of a jet impinging into a trough- like shaped cavity is discussed; the investigation is performed both experimentally and numerically. The unsteady character of this flow is considered a result of instability in otherwise symmetrical flow- field. The mechanism of the jet swinging is then identified as an action of the Coanda effect between a jet and a quasi- wall- jet.
Pasivní a aktivní metody řízení mezní vrstvy
Matějka, Milan ; Popelka, Lukáš
The paper deals with influence of the passive and active method of control on the flow field. It is well known fact that boundary layer separation has a fundamental effect on aircraft airfoil performance, compressors and turbines performance and other bodies, subject to study of internal and external aerodynamics. By the boundary layer control, it is possible to obtain both operational economy and extension of efficient operational region. Traditional methods of active boundary layer control are very complex and their application needs complex facilities. Modern methods based on the control by synthetic jets or plasma actuator are simpler, but their design has to be carried out at rather well experience and detailed knowledge about boundary layer and its interaction with the actuator.
Řízení mezní vrstvy na obtékaném profilu a vliv turbulence vnějšího proudu
Popelka, Lukáš ; Matějka, M.
The article deals with numerical and experimental investigation of boundary layer transition, separation bubbles and flow control on sailplane airfoils with respect to outer stream turbulence.
Heat loss of the hot-wire at low overheats
Antoš, Pavel
Collis-Williams cooling law seems not to be suitable for a wide range of the operation wire temperatures. A new form of the cooling law has been proposed for low-overheated wires.
Experimentální studie vývoje povrchového tření během zkráceného přechodu do turbulence
Jonáš, Pavel ; Mazur, Oton ; Uruba, Václav
The authors clearly proved formerly that the length scale of the external turbulent flow influences the start and the end of boundary layer transition simultaneously with the velocity scale. An elaborated physical explanation why this happens is not yet available. So a conditional analysis of the wall-friction was performed in the region of transition to turbulence. A working hypothesis was formulated for the continuation of the research after the received results.
Reference Film Temperature in the Hot-wire Anemometry
Antoš, Pavel
Dimensionless parameters in the cooling law are referred to the reference film temperature. In case of the mean film temperature there is necessary to use a temperature loading factor. There were found such reference temperatures that the loading factor is eliminated.
Řízení vyfukováním odtrženého proudu v kanálu se schodovitým rozšířením
Jonáš, Pavel ; Mazur, Oton ; Uruba, Václav
This paper is concerned with prospects of control of narrow channel flow behind a backward-facing step by blowing / suction near the step foot. The slots differ in both the orifice shape (rectangle or serrated) and area of its cross-section.

National Repository of Grey Literature : 28 records found   beginprevious19 - 28  jump to record:
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