Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays

The desire to achieve higher heat transfer augmentation for turbine blades is fueled by the increased power output and efficiency that is achievable with high turbine inlet temperatures. The use of internal cooling channels fitted with pin fin arrays serves as one method of accomplishing this goal....

Full description

Bibliographic Details
Main Author: Thrift, Alan Albright
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/31189
http://scholar.lib.vt.edu/theses/available/etd-02092007-143711/
id ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-31189
record_format oai_dc
spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-311892020-09-26T05:38:39Z Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays Thrift, Alan Albright Mechanical Engineering Thole, Karen A. Paul, Mark R. Dancey, Clinton L. force measurement lift cylinder drag pin fin internal cooling pressure drop The desire to achieve higher heat transfer augmentation for turbine blades is fueled by the increased power output and efficiency that is achievable with high turbine inlet temperatures. The use of internal cooling channels fitted with pin fin arrays serves as one method of accomplishing this goal. Consequently, the addition of pin fin arrays comes at the expense of increased pressure drop. Therefore the pin fin geometry must be judiciously chosen to achieve the required heat transfer rate while minimizing the associated pressure drop. <p> This project culminates in the measurement of both pin fin force and array pressure drop as they related to changes in the array geometry. Specifically, the effects of Reynolds number, spanwise pin spacing, streamwise pin spacing, pin aspect ratio, and flow incidence angle. Direct two-component force measurement is achieved with a cantilever beam force sensor that uses highly sensitive piezoresistive strain gauges, relating the strain at the base of the beam to the applied force. With proper characterization, forces as small as one-tenth the weight of a paper clip are successfully measured. Additionally, array pressure drop measurements are achieved using static pressure taps. <p> Experiments were conducted over a range of Reynolds numbers between 7,500 and 35,000. Changes in the spanwise pin spacing were shown to substantially alter the pin fin drag and array pressure drop, while changes in the streamwise pin spacing were less influential. The experimental results also showed a dramatic reduction in the pin fin drag and array pressure drop for an inline flow incidence angle. Finally, changes in the pin aspect ratio were shown to have little effect on the array pressure drop. Master of Science 2014-03-14T20:31:39Z 2014-03-14T20:31:39Z 2007-02-09 2007-02-09 2010-10-27 2007-02-20 Thesis etd-02092007-143711 http://hdl.handle.net/10919/31189 http://scholar.lib.vt.edu/theses/available/etd-02092007-143711/ Thesis_ETD2.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ application/pdf Virginia Tech
collection NDLTD
format Others
sources NDLTD
topic force measurement
lift
cylinder drag
pin fin
internal cooling
pressure drop
spellingShingle force measurement
lift
cylinder drag
pin fin
internal cooling
pressure drop
Thrift, Alan Albright
Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays
description The desire to achieve higher heat transfer augmentation for turbine blades is fueled by the increased power output and efficiency that is achievable with high turbine inlet temperatures. The use of internal cooling channels fitted with pin fin arrays serves as one method of accomplishing this goal. Consequently, the addition of pin fin arrays comes at the expense of increased pressure drop. Therefore the pin fin geometry must be judiciously chosen to achieve the required heat transfer rate while minimizing the associated pressure drop. <p> This project culminates in the measurement of both pin fin force and array pressure drop as they related to changes in the array geometry. Specifically, the effects of Reynolds number, spanwise pin spacing, streamwise pin spacing, pin aspect ratio, and flow incidence angle. Direct two-component force measurement is achieved with a cantilever beam force sensor that uses highly sensitive piezoresistive strain gauges, relating the strain at the base of the beam to the applied force. With proper characterization, forces as small as one-tenth the weight of a paper clip are successfully measured. Additionally, array pressure drop measurements are achieved using static pressure taps. <p> Experiments were conducted over a range of Reynolds numbers between 7,500 and 35,000. Changes in the spanwise pin spacing were shown to substantially alter the pin fin drag and array pressure drop, while changes in the streamwise pin spacing were less influential. The experimental results also showed a dramatic reduction in the pin fin drag and array pressure drop for an inline flow incidence angle. Finally, changes in the pin aspect ratio were shown to have little effect on the array pressure drop. === Master of Science
author2 Mechanical Engineering
author_facet Mechanical Engineering
Thrift, Alan Albright
author Thrift, Alan Albright
author_sort Thrift, Alan Albright
title Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays
title_short Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays
title_full Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays
title_fullStr Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays
title_full_unstemmed Aerodynamic Force and Pressure Loss Measurements on Low Aspect Ratio Pin Fin Arrays
title_sort aerodynamic force and pressure loss measurements on low aspect ratio pin fin arrays
publisher Virginia Tech
publishDate 2014
url http://hdl.handle.net/10919/31189
http://scholar.lib.vt.edu/theses/available/etd-02092007-143711/
work_keys_str_mv AT thriftalanalbright aerodynamicforceandpressurelossmeasurementsonlowaspectratiopinfinarrays
_version_ 1719342563887939584