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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
1

Advance LDA techniques for measurement of 3D boundary layer velocity profiles on a helicopter rotor

Swales, Christopher January 1994 (has links)
No description available.
2

Boundary layer instability noise on aerofoils

Nash, Emma Clare January 1996 (has links)
No description available.
3

Experimental and Numerical Investigations of Velocity and Turbulent Quantities of a Jet Diffusion Flame

Piro, Markus Hans 10 October 2007 (has links)
A turbulent diffusion flame that is typically used in a thermal spray coating system was analyzed in this study, as part of a diagnostic and development program undertaken by a research group at Queen’s University. Contributions made by this researcher were to numerically and experimentally investigate velocity and turbulent fields of the gaseous phase of the jet. Numerical and experimental analyses have been further developed upon previous research, with improved numerical methods and advanced experimental instrumentation. Numerous numerical simulations were performed in both two dimensional axisymmetric and three dimensional wedge geometries, while testing the dependence of the final solution on various physical models. Numerical analyses revealed the requirement for simulating this problem in three dimensions and improved turbulence modeling to account for relatively high levels of anisotropy. Velocity and turbulent measurements of non-reacting and combusting jets were made with a laser Doppler anemometer to validate numerical models. Excellent agreement was found between predicted and measured velocity and turbulent quantities for cold flow cases. However, numerical predictions did not agree quite as well with experiments of the flame due to limitations in modeling techniques and flow tracking abilities of tracer particles used in experimentation. / Thesis (Master, Mechanical and Materials Engineering) -- Queen's University, 2007-09-28 13:05:54.365
4

DATA ANALYSIS OF TWO NON-ISOTHERMAL TURBULENT JETS

Quach, Dan 09 1900 (has links)
A three-component Laser Doppler Anemometer (LDA) instrument, an array of stationary thermocouples and a moving thermocouple were used to capture the three-dimensional flow and temperature fields for the system of two opposing axisymmetric turbulent jets. It was found that buoyancy-induced curvature of the hot jet resulted in cross shearing with the opposing jet. The following report will investigate the adequacy of the current experimental measurements for the identification of coherent structures and the characterization of their effects on the mean flow. Identification tools include the power spectra and conditional average velocity measurements based on the Window Average Gradient (WAG). It was determined that the low sampling and large spatial positions of the thermocouple measurements were not for the retrieval of quantitative turbulence data. For the velocity measurements, the LDA data were found to be adequate in regions of low turbulence intensities but degraded as the measurements approached the region where the two jet shear layers interacted. The detection of periodic structures from the power spectrum was inconclusive due to noise. The WAG algorithm was affected by the irregular sampling and required modification. For the events detected, an intermittency factor of 16.4% at the interaction region of two shear layers was observed. In addition, these results suggest that these events contribute 30% of the mean momentum transfer across the jet. Furthermore, the contribution of these events to the lateral component of the turbulent kinetic energy was nearly eight times larger than the contributions to the axial or transverse direction. / Thesis / Master of Engineering (ME)
5

A study of sediment transport in two-stage meandering channel

Chan, Tuck Leong January 2003 (has links)
An investigation of the flow characteristics and sediment transport processes has been carried out in a two-stage meandering channel. Three phases of experiments have been conducted with various floodplain roughnesses. The dimensions of the flume are 13m long and 2.4m wide with a fixed valley slope of 11500. The meandering main channel has a sinuosity of 1.384 with top width of 0.4m. In each phase of the experiment, hydraulic data pertaining to stage-discharge, bed topography and sediment transport rate were measured at various overbank flow depths. Several flow depths were chosen to measure the three-dimensional velocities by means of Laser Doppler Anemometer and the morphological bedforms were recorded using the Photogrammetric technique. The boundary shear stresses were also measured by means of a Preston Tube and Vane Indicator. The experimental results showed that the presence of the energy losses due to momentum exchange and turbulence, bedforms roughness and floodplain roughness induced additional flow resistance to the main channel flow, particularly for shallow overbank flows. The combination of these losses affected a significant reduction in velocity and boundary shear stress in the main channel which, subsequently led to the reduction of sediment discharge at low relative depth for most tested cases. The reduction was more pronounced when the floodplain roughness increased. The examination of the three-dimensional velocity indicated that the formation of bedforms in the main channel is significantly affected by the flow structures, especially the secondary flow. A new method for predicting velocity and sediment transport rate has been introduced based on the two-dimensional equation (Spooner's) coupled with the self-calibrated empirical transport formula. The proposed method gave accurate prediction for depthaveraged velocity and sediment transport rate for two-stage meandering channel.

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