Effect of chordwise flexibility on flapping wing aerodynamics

Onur Son; Oksan Cetiner

doi:10.1007/978-3-319-30602-5_26

Effect of chordwise flexibility on flapping wing aerodynamics

Onur Son^*
, Oksan Cetiner

^*Bu çalışma için yazışmadan sorumlu yazar

Uzay Mühendisliği Bölümü

Istanbul Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

1 Atıf (Scopus)

Özet

In this study, the effect of chordwise flexibility has been investigated experimentally for a plunging foil. A Digital Particle Image Velocimetry (DPIV) system is used to determine instantaneous velocity and vorticity fields around and in the near-wake of the wings in conjunction with simultaneous direct force/moment measurements. The aerodynamic/hydrodynamic performance is studied for rigid and flexible wings undergoing plunge motion at different amplitudes and frequencies in a freestream of Re = 10 000. The thrust coefficient (C_T), the power input coefficient (C_P) and the efficiency (η) values are also obtained and linked with the flexibility, trailing edge motion and flow structures in the near-wake.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF 2015
Editörler	Antonio Segalini
Yayınlayan	Springer Science and Business Media, LLC
Sayfalar	203-210
Sayfa sayısı	8
ISBN (Basılı)	9783319306001
DOI'lar	https://doi.org/10.1007/978-3-319-30602-5_26
Yayın durumu	Yayınlandı - 2016
Etkinlik	5th International Conference on Jets, Wakes and Separated Flows, ICJWSF2015 - Stockholm, Sweden Süre: 15 Haz 2015 → 18 Haz 2015

Yayın serisi

Adı	Springer Proceedings in Physics
Hacim	185
ISSN (Basılı)	0930-8989
ISSN (Elektronik)	1867-4941

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	5th International Conference on Jets, Wakes and Separated Flows, ICJWSF2015
Ülke/Bölge	Sweden
Şehir	Stockholm
Periyot	15/06/15 → 18/06/15

Bibliyografik not

Publisher Copyright:
© Springer International Publishing Switzerland 2016.

Finansman

The authors acknowledge the funding provided by the Scientific and Technological Research Council of Turkey (TUBITAK) Grant 112M682.

Finansörler	Finansör numarası
TUBITAK	112M682
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu

Belgeye Erişim

10.1007/978-3-319-30602-5_26

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

@inproceedings{1b1c4d6b7fb046bfb850357c557c7340,

title = "Effect of chordwise flexibility on flapping wing aerodynamics",

abstract = "In this study, the effect of chordwise flexibility has been investigated experimentally for a plunging foil. A Digital Particle Image Velocimetry (DPIV) system is used to determine instantaneous velocity and vorticity fields around and in the near-wake of the wings in conjunction with simultaneous direct force/moment measurements. The aerodynamic/hydrodynamic performance is studied for rigid and flexible wings undergoing plunge motion at different amplitudes and frequencies in a freestream of Re = 10 000. The thrust coefficient (CT), the power input coefficient (CP) and the efficiency (η) values are also obtained and linked with the flexibility, trailing edge motion and flow structures in the near-wake.",

author = "Onur Son and Oksan Cetiner",

note = "Publisher Copyright: {\textcopyright} Springer International Publishing Switzerland 2016.; 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF2015 ; Conference date: 15-06-2015 Through 18-06-2015",

year = "2016",

doi = "10.1007/978-3-319-30602-5\_26",

language = "English",

isbn = "9783319306001",

series = "Springer Proceedings in Physics",

publisher = "Springer Science and Business Media, LLC",

pages = "203--210",

editor = "Antonio Segalini",

booktitle = "Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF 2015",

address = "United States",

}

Son, O & Cetiner, O 2016, Effect of chordwise flexibility on flapping wing aerodynamics. in A Segalini (ed.), Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF 2015. Springer Proceedings in Physics, hac. 185, Springer Science and Business Media, LLC, pp. 203-210, 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF2015, Stockholm, Sweden, 15/06/15. https://doi.org/10.1007/978-3-319-30602-5_26

Effect of chordwise flexibility on flapping wing aerodynamics. / Son, Onur; Cetiner, Oksan.
Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF 2015. ed. / Antonio Segalini. Springer Science and Business Media, LLC, 2016. p. 203-210 (Springer Proceedings in Physics; Hac. 185).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - Effect of chordwise flexibility on flapping wing aerodynamics

AU - Son, Onur

AU - Cetiner, Oksan

PY - 2016

Y1 - 2016

N2 - In this study, the effect of chordwise flexibility has been investigated experimentally for a plunging foil. A Digital Particle Image Velocimetry (DPIV) system is used to determine instantaneous velocity and vorticity fields around and in the near-wake of the wings in conjunction with simultaneous direct force/moment measurements. The aerodynamic/hydrodynamic performance is studied for rigid and flexible wings undergoing plunge motion at different amplitudes and frequencies in a freestream of Re = 10 000. The thrust coefficient (CT), the power input coefficient (CP) and the efficiency (η) values are also obtained and linked with the flexibility, trailing edge motion and flow structures in the near-wake.

AB - In this study, the effect of chordwise flexibility has been investigated experimentally for a plunging foil. A Digital Particle Image Velocimetry (DPIV) system is used to determine instantaneous velocity and vorticity fields around and in the near-wake of the wings in conjunction with simultaneous direct force/moment measurements. The aerodynamic/hydrodynamic performance is studied for rigid and flexible wings undergoing plunge motion at different amplitudes and frequencies in a freestream of Re = 10 000. The thrust coefficient (CT), the power input coefficient (CP) and the efficiency (η) values are also obtained and linked with the flexibility, trailing edge motion and flow structures in the near-wake.

UR - https://www.scopus.com/pages/publications/84978975983

U2 - 10.1007/978-3-319-30602-5_26

DO - 10.1007/978-3-319-30602-5_26

M3 - Conference contribution

AN - SCOPUS:84978975983

SN - 9783319306001

T3 - Springer Proceedings in Physics

SP - 203

EP - 210

BT - Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF 2015

A2 - Segalini, Antonio

PB - Springer Science and Business Media, LLC

T2 - 5th International Conference on Jets, Wakes and Separated Flows, ICJWSF2015

Y2 - 15 June 2015 through 18 June 2015

ER -

Effect of chordwise flexibility on flapping wing aerodynamics

Özet

Yayın serisi

???event.eventtypes.event.conference???

Bibliyografik not

Finansman

Belgeye Erişim

Diğer Dosyalar ve Linkler

Parmak izi

Alıntı Yap