author_facet Bose, Chandan
Sarkar, Sunetra
Gupta, Sayan
Bose, Chandan
Sarkar, Sunetra
Gupta, Sayan
author Bose, Chandan
Sarkar, Sunetra
Gupta, Sayan
spellingShingle Bose, Chandan
Sarkar, Sunetra
Gupta, Sayan
MATEC Web of Conferences
Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
author_sort bose, chandan
spelling Bose, Chandan Sarkar, Sunetra Gupta, Sayan 2261-236X EDP Sciences http://dx.doi.org/10.1051/matecconf/201814808001 <jats:p>The present paper investigates the effects of noisy flow fluctuations on the fluid-structure interaction (FSI) behaviour of a span-wise flexible wing modelled as a two degree-of-freedom elastically mounted flapping airfoil. In the sterile flow conditions, the system undergoes a Hopf bifurcation as the free-stream velocity exceeds a critical limit resulting in a stable limit-cycle oscillation (LCO) from a fixed point response. On the other hand, the qualitative dynamics changes from a stochastic fixed point to a random LCO through an intermittent state in the presence of irregular flow fluctuations. The probability density function depicts the most probable system state in the phase space. A phenomenological bifurcation (P-bifurcation) analysis based on the transition in the topology associated with the structure of the joint probability density function (pdf) of the response variables has been carried out. The joint pdf corresponding to the stochastic fixed point possesses a Dirac delta function like structure with a sharp single peak around zero. As the mean flow speed crosses the critical value, the joint pdf bifurcates to a crater-like structure indicating the occurrence of a P-bifurcation. The intermittent state is characterized by the co-existence of the unimodal as well as the crater like structure.</jats:p> Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil MATEC Web of Conferences
doi_str_mv 10.1051/matecconf/201814808001
facet_avail Online
Free
format ElectronicArticle
fullrecord blob:ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuMTA1MS9tYXRlY2NvbmYvMjAxODE0ODA4MDAx
id ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuMTA1MS9tYXRlY2NvbmYvMjAxODE0ODA4MDAx
institution DE-Gla1
DE-Zi4
DE-15
DE-Pl11
DE-Rs1
DE-105
DE-14
DE-Ch1
DE-L229
DE-D275
DE-Bn3
DE-Brt1
DE-D161
DE-Zwi2
imprint EDP Sciences, 2018
imprint_str_mv EDP Sciences, 2018
issn 2261-236X
issn_str_mv 2261-236X
language Undetermined
mega_collection EDP Sciences (CrossRef)
match_str bose2018stochasticbifurcationanalysisofanelasticallymountedflappingairfoil
publishDateSort 2018
publisher EDP Sciences
recordtype ai
record_format ai
series MATEC Web of Conferences
source_id 49
title Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_unstemmed Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_full Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_fullStr Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_full_unstemmed Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_short Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_sort stochastic bifurcation analysis of an elastically mounted flapping airfoil
url http://dx.doi.org/10.1051/matecconf/201814808001
publishDate 2018
physical 08001
description <jats:p>The present paper investigates the effects of noisy flow fluctuations on the fluid-structure interaction (FSI) behaviour of a span-wise flexible wing modelled as a two degree-of-freedom elastically mounted flapping airfoil. In the sterile flow conditions, the system undergoes a Hopf bifurcation as the free-stream velocity exceeds a critical limit resulting in a stable limit-cycle oscillation (LCO) from a fixed point response. On the other hand, the qualitative dynamics changes from a stochastic fixed point to a random LCO through an intermittent state in the presence of irregular flow fluctuations. The probability density function depicts the most probable system state in the phase space. A phenomenological bifurcation (P-bifurcation) analysis based on the transition in the topology associated with the structure of the joint probability density function (pdf) of the response variables has been carried out. The joint pdf corresponding to the stochastic fixed point possesses a Dirac delta function like structure with a sharp single peak around zero. As the mean flow speed crosses the critical value, the joint pdf bifurcates to a crater-like structure indicating the occurrence of a P-bifurcation. The intermittent state is characterized by the co-existence of the unimodal as well as the crater like structure.</jats:p>
container_start_page 0
container_title MATEC Web of Conferences
container_volume 148
format_de105 Article, E-Article
format_de14 Article, E-Article
format_de15 Article, E-Article
format_de520 Article, E-Article
format_de540 Article, E-Article
format_dech1 Article, E-Article
format_ded117 Article, E-Article
format_degla1 E-Article
format_del152 Buch
format_del189 Article, E-Article
format_dezi4 Article
format_dezwi2 Article, E-Article
format_finc Article, E-Article
format_nrw Article, E-Article
_version_ 1792320963094773771
geogr_code not assigned
last_indexed 2024-03-01T10:54:28.165Z
geogr_code_person not assigned
openURL url_ver=Z39.88-2004&ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fvufind.svn.sourceforge.net%3Agenerator&rft.title=Stochastic+Bifurcation+Analysis+of+an+Elastically+Mounted+Flapping+Airfoil&rft.date=2018-01-01&genre=article&issn=2261-236X&volume=148&pages=08001&jtitle=MATEC+Web+of+Conferences&atitle=Stochastic+Bifurcation+Analysis+of+an+Elastically+Mounted+Flapping+Airfoil&aulast=Gupta&aufirst=Sayan&rft_id=info%3Adoi%2F10.1051%2Fmatecconf%2F201814808001&rft.language%5B0%5D=und
SOLR
_version_ 1792320963094773771
author Bose, Chandan, Sarkar, Sunetra, Gupta, Sayan
author_facet Bose, Chandan, Sarkar, Sunetra, Gupta, Sayan, Bose, Chandan, Sarkar, Sunetra, Gupta, Sayan
author_sort bose, chandan
container_start_page 0
container_title MATEC Web of Conferences
container_volume 148
description <jats:p>The present paper investigates the effects of noisy flow fluctuations on the fluid-structure interaction (FSI) behaviour of a span-wise flexible wing modelled as a two degree-of-freedom elastically mounted flapping airfoil. In the sterile flow conditions, the system undergoes a Hopf bifurcation as the free-stream velocity exceeds a critical limit resulting in a stable limit-cycle oscillation (LCO) from a fixed point response. On the other hand, the qualitative dynamics changes from a stochastic fixed point to a random LCO through an intermittent state in the presence of irregular flow fluctuations. The probability density function depicts the most probable system state in the phase space. A phenomenological bifurcation (P-bifurcation) analysis based on the transition in the topology associated with the structure of the joint probability density function (pdf) of the response variables has been carried out. The joint pdf corresponding to the stochastic fixed point possesses a Dirac delta function like structure with a sharp single peak around zero. As the mean flow speed crosses the critical value, the joint pdf bifurcates to a crater-like structure indicating the occurrence of a P-bifurcation. The intermittent state is characterized by the co-existence of the unimodal as well as the crater like structure.</jats:p>
doi_str_mv 10.1051/matecconf/201814808001
facet_avail Online, Free
format ElectronicArticle
format_de105 Article, E-Article
format_de14 Article, E-Article
format_de15 Article, E-Article
format_de520 Article, E-Article
format_de540 Article, E-Article
format_dech1 Article, E-Article
format_ded117 Article, E-Article
format_degla1 E-Article
format_del152 Buch
format_del189 Article, E-Article
format_dezi4 Article
format_dezwi2 Article, E-Article
format_finc Article, E-Article
format_nrw Article, E-Article
geogr_code not assigned
geogr_code_person not assigned
id ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuMTA1MS9tYXRlY2NvbmYvMjAxODE0ODA4MDAx
imprint EDP Sciences, 2018
imprint_str_mv EDP Sciences, 2018
institution DE-Gla1, DE-Zi4, DE-15, DE-Pl11, DE-Rs1, DE-105, DE-14, DE-Ch1, DE-L229, DE-D275, DE-Bn3, DE-Brt1, DE-D161, DE-Zwi2
issn 2261-236X
issn_str_mv 2261-236X
language Undetermined
last_indexed 2024-03-01T10:54:28.165Z
match_str bose2018stochasticbifurcationanalysisofanelasticallymountedflappingairfoil
mega_collection EDP Sciences (CrossRef)
physical 08001
publishDate 2018
publishDateSort 2018
publisher EDP Sciences
record_format ai
recordtype ai
series MATEC Web of Conferences
source_id 49
spelling Bose, Chandan Sarkar, Sunetra Gupta, Sayan 2261-236X EDP Sciences http://dx.doi.org/10.1051/matecconf/201814808001 <jats:p>The present paper investigates the effects of noisy flow fluctuations on the fluid-structure interaction (FSI) behaviour of a span-wise flexible wing modelled as a two degree-of-freedom elastically mounted flapping airfoil. In the sterile flow conditions, the system undergoes a Hopf bifurcation as the free-stream velocity exceeds a critical limit resulting in a stable limit-cycle oscillation (LCO) from a fixed point response. On the other hand, the qualitative dynamics changes from a stochastic fixed point to a random LCO through an intermittent state in the presence of irregular flow fluctuations. The probability density function depicts the most probable system state in the phase space. A phenomenological bifurcation (P-bifurcation) analysis based on the transition in the topology associated with the structure of the joint probability density function (pdf) of the response variables has been carried out. The joint pdf corresponding to the stochastic fixed point possesses a Dirac delta function like structure with a sharp single peak around zero. As the mean flow speed crosses the critical value, the joint pdf bifurcates to a crater-like structure indicating the occurrence of a P-bifurcation. The intermittent state is characterized by the co-existence of the unimodal as well as the crater like structure.</jats:p> Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil MATEC Web of Conferences
spellingShingle Bose, Chandan, Sarkar, Sunetra, Gupta, Sayan, MATEC Web of Conferences, Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_full Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_fullStr Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_full_unstemmed Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_short Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
title_sort stochastic bifurcation analysis of an elastically mounted flapping airfoil
title_unstemmed Stochastic Bifurcation Analysis of an Elastically Mounted Flapping Airfoil
url http://dx.doi.org/10.1051/matecconf/201814808001