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Finite Element Vibration Modeling an...
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ProQuest Information and Learning Co.
Finite Element Vibration Modeling and Experimental Validation for an Aircraft Engine Casing.
Record Type:
Language materials, manuscript : Monograph/item
Title/Author:
Finite Element Vibration Modeling and Experimental Validation for an Aircraft Engine Casing./
Author:
Rabbitt, Christopher.
Description:
1 online resource (97 pages)
Notes:
Source: Masters Abstracts International, Volume: 57-02.
Contained By:
Masters Abstracts International57-02(E).
Subject:
Mechanical engineering. -
Online resource:
click for full text (PQDT)
ISBN:
9780355452518
Finite Element Vibration Modeling and Experimental Validation for an Aircraft Engine Casing.
Rabbitt, Christopher.
Finite Element Vibration Modeling and Experimental Validation for an Aircraft Engine Casing.
- 1 online resource (97 pages)
Source: Masters Abstracts International, Volume: 57-02.
Thesis (M.A.S.)--University of Toronto (Canada), 2017.
Includes bibliographical references
This thesis presents a procedure for the development and validation of a theoretical vibration model, applies this procedure to a pair of aircraft engine casings, and compares select parameters from experimental testing of those casings to those from a theoretical model using the Modal Assurance Criterion (MAC) and linear regression coefficients. A novel method of determining the optimal MAC between axisymmetric results is developed and employed.
Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2018
Mode of access: World Wide Web
ISBN: 9780355452518Subjects--Topical Terms:
557493
Mechanical engineering.
Index Terms--Genre/Form:
554714
Electronic books.
Finite Element Vibration Modeling and Experimental Validation for an Aircraft Engine Casing.
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Finite Element Vibration Modeling and Experimental Validation for an Aircraft Engine Casing.
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Adviser: Kamran Behdinan.
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Thesis (M.A.S.)--University of Toronto (Canada), 2017.
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Includes bibliographical references
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This thesis presents a procedure for the development and validation of a theoretical vibration model, applies this procedure to a pair of aircraft engine casings, and compares select parameters from experimental testing of those casings to those from a theoretical model using the Modal Assurance Criterion (MAC) and linear regression coefficients. A novel method of determining the optimal MAC between axisymmetric results is developed and employed.
520
$a
It is concluded that the dynamic finite element models developed as part of this research are fully capable of modelling the modal parameters within the frequency range of interest. Confidence intervals calculated in this research for correlation coefficients provide important information regarding the reliability of predictions, and it is recommended that these intervals be calculated for all comparable coefficients. The procedure outlined for aligning mode shapes around an axis of symmetry proved useful, and the results are promising for the development of further optimization techniques.
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2018
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Mode of access: World Wide Web
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click for full text (PQDT)
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