AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES

Ph.D

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Bibliographic Details
Main Author:	YU QIJING
Other Authors:	MECHANICAL ENGINEERING
Format:	Theses and Dissertations
Language:	English
Published:	2020
Subjects:	Aeroelasticity, Flutter, Limit Cycle Oscillation, Aircraft Wing, Structural Nonlinearities
Online Access:	https://scholarbank.nus.edu.sg/handle/10635/167807
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Institution:	National University of Singapore
Language:	English

id	sg-nus-scholar.10635-167807
record_format	dspace
spelling	sg-nus-scholar.10635-1678072021-06-02T13:13:29Z AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES YU QIJING MECHANICAL ENGINEERING Boo Cheong Khoo Aeroelasticity, Flutter, Limit Cycle Oscillation, Aircraft Wing, Structural Nonlinearities Ph.D DOCTOR OF PHILOSOPHY (FOE) 2020-05-06T18:00:29Z 2020-05-06T18:00:29Z 2020-01-17 Thesis YU QIJING (2020-01-17). AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES. ScholarBank@NUS Repository. https://scholarbank.nus.edu.sg/handle/10635/167807 en
institution	National University of Singapore
building	NUS Library
continent	Asia
country	Singapore Singapore
content_provider	NUS Library
collection	ScholarBank@NUS
language	English
topic	Aeroelasticity, Flutter, Limit Cycle Oscillation, Aircraft Wing, Structural Nonlinearities
spellingShingle	Aeroelasticity, Flutter, Limit Cycle Oscillation, Aircraft Wing, Structural Nonlinearities YU QIJING AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES
description	Ph.D
author2	MECHANICAL ENGINEERING
author_facet	MECHANICAL ENGINEERING YU QIJING
format	Theses and Dissertations
author	YU QIJING
author_sort	YU QIJING
title	AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES
title_short	AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES
title_full	AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES
title_fullStr	AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES
title_full_unstemmed	AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES
title_sort	aeroelastic limit cycle oscillation analysis of aircraft wing with multiple structural nonlinearities
publishDate	2020
url	https://scholarbank.nus.edu.sg/handle/10635/167807
_version_	1702431021038829568

AEROELASTIC LIMIT CYCLE OSCILLATION ANALYSIS OF AIRCRAFT WING WITH MULTIPLE STRUCTURAL NONLINEARITIES

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