Development and application of transition detection using infrared thermography for characterization of fan blade waviness effects
Name
1191824172-MIT.pdf
Size
30.22 MB
Format
Adobe PDF
Checksum (MD5)
658117869de88dd3415173ee1a0a0c2e
Author(s)
Ramaswamy, Vaishnavi,S. M.Massachusetts Institute of Technology.
Advisor(s)
Zoltán S. Spakovszky and Edward M. Greitzer.
Date Issued
2020
Publisher
Massachusetts Institute of Technology
Abstract
This thesis describes a new approach to infrared measurement of boundary layer transition and its implementation in a natural transition experiment on flat and wavy surfaces. The approach relies on computing the convective heat transfer coefficient field on the test surface and inferring transition region from the same. The transition location identified from infrared images is assessed against hotwire measurement which establishes transition location based on the growth of Tollmien-Schlichting waves in the boundary layer. Infrared thermography is used to determine the effects of surface waviness on natural transition in the regime of operation of civil aero engine fan blades. Surface waviness on fan blades arises from the carbon composite manufacturing process. The waviness results in transition point movement due to receptivity amplification between the surface wavelength and Tollmien-Schlichting wavelength, as recently described by Lee [17]. The research, therefore, develops and assesses an improved method for field measurement of transition from infrared images and captures the transition point movement due to surface waviness. The infrared transition detection technique developed here shows good agreement with midspan hotwire measurements (within 5% of chord) for natural transition experiments on a flat plate. Previous infrared based transition inference methods are shown to deviate from hotwire measurements by ~ 30% of chord. The research demonstrates spanwise uniformity in transition location and transition point movement (spanwise variation within 10% of chord) for the experimental configuration, and thereby characterizes the effect of surface waviness on natural transition for a representative fan blade.
Description
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, May, 2020
Cataloged from the official PDF of thesis.
Includes bibliographical references (pages 144-148).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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