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  • 1
    ISSN: 1432-1114
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract In this paper we address the effectiveness of riblets on skin friction reduction under the influence of an adverse pressure gradient. The measurements were taken in a wind tunnel. Skin friction was observed with a drag balance which has a reproducibility of better than 1%. The accuracy of the balance is estimated to be less than 1% for the case of zero-pressure gradient and at most 3% for a pressure gradient. The data on skin friction reduction at zero pressure gradient were consistent with previous results and amount to 5% at dimensionless riblet width of s + = 13. We find that at all adverse pressure gradients the skin friction reduction by riblets persists. At moderate pressure gradients the reduction increases somewhat to 7%. The velocity profile which is also measured, exhibits the characteristic shape for a boundary layer with an adverse pressure gradient and agrees well with theory. From the velocity profiles measured at two stations we estimated with the help of a momentum balance the skin friction and skin friction reduction. The results differ from the drag-balance data. Due to the poor accuracy of the momentum balance method which we estimate in our case, we conclude that the results obtained with this method are less reliable than those obtained with the drag balance. This throws some doubt on previous results on drag reduction under the influence of a pressure gradient which were based on the momentum balance method.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Flow, turbulence and combustion 31 (1975), S. 343-362 
    ISSN: 1573-1987
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract Measurements have been made of the distributions of the mean-velocity and the axial turbulence velocity component in a cross-section of a circular tube at various distances downstream from a number of different constrictions. Also spectral distributions of the turbulence velocity have been measured in the axis of the tube and in a point very close to the wall. The constrictions had a contraction ratio of 0.25 except one which had a ratio of 0.5. One of the constrictions was made of a thin rubber hose. When for this constriction the contraction ratio was reduced to a value smaller than 0.25, self-excited vibrations of the hose took place, producing an oscillating flow of the air in the tube. The Reynoldsnumber was kept at roughly 5,000. As could be expected, after 40 tube diameter distance downstream from the constrictions an almost complete recovery of the disturbed turbulent flow, as far as the distributions of the mean velocity and relative turbulence intensity are concerned, was obtained. Depending on the shape of the constriction even a shorter distance appeared to be sufficient. The flexible constriction then was in the non-vibrating condition. However, the spectral distributions showed in some cases still a difference with the undisturbed case, in particular in the low frequency range. If the flexible constriction was vibrating, the induced oscillations of the flow which showed up as discrete peaks in the spectral distributions, persisted over the entire length of the tube, again as expected.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    Springer
    Flow, turbulence and combustion 40 (1983), S. 355-375 
    ISSN: 1573-1987
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract The development region of a free round turbulent jet was experimentally investigated in order to determine the dependence of the jet development on the exit conditions. In particular the influence of the exit conditions on the entrainment rate in both the axisymmetrix mixing layer region and at a distance of 20D from the nozzle was investigated. The entrainment rate at 20D depends noticeably on the exit boundary layer state, i.e. laminar or turbulent, and on the turbulence intensity of the core. A laminar exit boundary layer showed the highest value of entrainment rate. A turbulent one reduced the entrainment rate at 20D by 15%. A grid placed at the nozzle exit, in order to increase the turbulence intensity of the core, reduced the entrainment rate at 20D by 40%. It must be mentioned that this grid also disturbed the exit boundary layer. An empirical relation for the entrainment rate at the end of the mixing layer region as a function of the mixing layer parameters, is successful in predicting the entrainment rate at 20D within an accuracy of 5%. This result suggests a strong dependence of the jet development region on mixing layer processes, i.e. the development of organized structures and their coalescence. Possibly there is no asymptotic region which is fully independent of the mixing layer processes, and which is not more or less influenced by the exit conditions via the influence on these processes.
    Type of Medium: Electronic Resource
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