The Development of a New High Aspect-Ratio Turbulent Channel Flow Facility

University essay from KTH/Strömningsmekanik och Teknisk Akustik

Author: Agastya Parikh; [2020]

Keywords: ;

Abstract: Turbulent channel flows are of great interest for investigations of modified wall boundary conditions due to their well-understood characteristics and their broad applicability. In a reversal of typical trends, they can often be more difficult to investigate experimentally than to simulate owing to the far-reaching influence of corner effects as well as the need for development lengths in excess of 200 channel half-heights in order to produce high-quality flow. In order to rovice experimental results to compare directly with current and future computational studies conducted in the FSG group, a new experimental channel flow facility has been designed for use with state-of-the-art optical measurement techniques such as planar and stereoscopic µPIV. To further aid in understanding the flows in and around complex surfaces, a water-NaI solution will be used as the working fluid for refractive-index matched experiments. A holistic design approach has been taken, taking into consideration design, manufacturing, operational, and experimental requirements and limitations. The facility has been designed with modularity as a key focus and the channel is subdivided into three interchangeable sections with the capability to support a wide range of experimental set-ups and configurations with minimal modification. To produce a high-quality flow, the channel has an aspect ratio of 20 : 1 and a development length of 288δ preceding the test section. Based on inital design estimates of pressure losses in the system, a 11 kW centrifugal pump has been specified and is projected to allow the channel to reach its maximum design flow velocity of 10 m s¯¹. Reτ of 2300 can be achieved, allowing for investigations well into the turbulent regime which remain within the range of Reynolds numbers that can be resolved in DNS studies.

  AT THIS PAGE YOU CAN DOWNLOAD THE WHOLE ESSAY. (follow the link to the next page)