Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme

Time integration is commonly used to obtain accurate system responses, such as the limit cycle oscillations (LCOs) for an aeroelastic system with freeplay. However, the integrations that start with various initial conditions (I.C.s) are usually studied case by case, so only a few system states can p...

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Main Authors: Xiangyu Wang, Zhigang Wu, Chao Yang
Format: Article
Language:English
Published: MDPI AG 2021-01-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/11/2/741
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spelling doaj-b0f04ef70feb4c7db35137f2955d906c2021-01-15T00:02:22ZengMDPI AGApplied Sciences2076-34172021-01-011174174110.3390/app11020741Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating SchemeXiangyu Wang0Zhigang Wu1Chao Yang2School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaTime integration is commonly used to obtain accurate system responses, such as the limit cycle oscillations (LCOs) for an aeroelastic system with freeplay. However, the integrations that start with various initial conditions (I.C.s) are usually studied case by case, so only a few system states can possibly be focused on. This paper proposes a state space iterating (SSI) scheme to find LCO solutions using time integration by using another method. First, a large number of arbitrary I.C. cases are used for time integrations, but only a very short integration time is required for each I.C. case. Second, system behaviors are depicted visually through a method that combines a modified Poincaré map and Lorenz map, in which the LCO solutions are found as fixed points via visual inspections. To verify the SSI scheme’s ability to find LCOs, a typical plunge–pitch wing section is established numerically. Time integrations with both the classic scheme and the proposed SSI scheme are carried out. The LCO results of the SSI scheme are well-aligned with those from the classic scheme. The SSI scheme visualizes the patterns of system responses using arbitrary I.C. cases and analyzes the LCO stability, which provides more mathematical insights into an aeroelastic system with freeplay.https://www.mdpi.com/2076-3417/11/2/741time integrationinitial conditionlimit cycle oscillationfreeplayPoincaré mapLorenz map
collection DOAJ
language English
format Article
sources DOAJ
author Xiangyu Wang
Zhigang Wu
Chao Yang
spellingShingle Xiangyu Wang
Zhigang Wu
Chao Yang
Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme
Applied Sciences
time integration
initial condition
limit cycle oscillation
freeplay
Poincaré map
Lorenz map
author_facet Xiangyu Wang
Zhigang Wu
Chao Yang
author_sort Xiangyu Wang
title Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme
title_short Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme
title_full Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme
title_fullStr Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme
title_full_unstemmed Integration of Freeplay-Induced Limit Cycles Based on a State Space Iterating Scheme
title_sort integration of freeplay-induced limit cycles based on a state space iterating scheme
publisher MDPI AG
series Applied Sciences
issn 2076-3417
publishDate 2021-01-01
description Time integration is commonly used to obtain accurate system responses, such as the limit cycle oscillations (LCOs) for an aeroelastic system with freeplay. However, the integrations that start with various initial conditions (I.C.s) are usually studied case by case, so only a few system states can possibly be focused on. This paper proposes a state space iterating (SSI) scheme to find LCO solutions using time integration by using another method. First, a large number of arbitrary I.C. cases are used for time integrations, but only a very short integration time is required for each I.C. case. Second, system behaviors are depicted visually through a method that combines a modified Poincaré map and Lorenz map, in which the LCO solutions are found as fixed points via visual inspections. To verify the SSI scheme’s ability to find LCOs, a typical plunge–pitch wing section is established numerically. Time integrations with both the classic scheme and the proposed SSI scheme are carried out. The LCO results of the SSI scheme are well-aligned with those from the classic scheme. The SSI scheme visualizes the patterns of system responses using arbitrary I.C. cases and analyzes the LCO stability, which provides more mathematical insights into an aeroelastic system with freeplay.
topic time integration
initial condition
limit cycle oscillation
freeplay
Poincaré map
Lorenz map
url https://www.mdpi.com/2076-3417/11/2/741
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AT zhigangwu integrationoffreeplayinducedlimitcyclesbasedonastatespaceiteratingscheme
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