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Massachusetts Institute of Technology

Probabilistic performance-based geometric tolerancing of compressor blades

Abstract

dc:description.abstract

The relationship between tolerances of statically measured geometric parameters and the aerodynamic performance of a sample of manufactured airfoils is investigated in this thesis. The objective is to determine which geometric parameters are the best discriminators of performance, and how these best discriminators are affected by changes in design methodology, manufacturing precision, and desired minimum performance levels. A probabilistic model of geometric variability for a three-dimensional blade is derived. Using this geometric variability model, probabilistic aerodynamic simulations are conducted to analyze the variability in aerodynamic performance. Tolerance optimization is then applied, in which allowable ranges for each geometric parameter are determined so as to maximize the quality of the accepted blades. Optimization is performed at several performance limits to observe how the effectiveness of tolerances and the best geometric discriminators of performance change with performance limit. A set of compressor blade data is used consisting of an original geometry, a deterministic re-design, and a probabilistic re-design. Using the geometric variability model, the variability is also artificially increased to investigate the impact of manufacturing precision on tolerance effectiveness. Results shows the best geometric indicators of performance are leading-edge thickness and measures pertaining to the curve quality of an airfoil. While design can affect the performance of tolerances, tolerances are no less effective on probabilistic designs than deterministic designs.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2005

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Lamb, Caroline Marie
Advisor dc:contributor.advisor
  • David L. Darmofal.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/32459
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/32459

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Lamb, Caroline Marie. Probabilistic performance-based geometric tolerancing of compressor blades. Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/32459