Full-Field Deformation Measurement of Morphing Wings

M. M. Mennu; B. Tran; P. G. Ifju; E. Santamaria

doi:10.1007/978-3-030-30028-9_16

Full-Field Deformation Measurement of Morphing Wings

M. M. Mennu, B. Tran, P. G. Ifju, E. Santamaria

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Scopus citations

Abstract

A micro air vehicle that can achieve a versatile flight condition is being designed. One way of achieving such versatility is through biomimicry. One aspect of this design utilizes a bird-like wing that changes shape to match four flight regimes; take-off-and -landing, cruise, high speed dash and one that enhances maneuverability. A joint mechanism using a tendon actuator between the inboard and the outboard portions of the wing is used to modify wing sweep. Macro fiber composites (MFCs) piezoelectric actuators in a bi-morph configuration are incorporated into the MAVs as control mechanism. Camber changes are implemented with tendon actuators. Finite element is used to model the wing section and perform a full-field deformation study and compared with experimental results. Digital image correlation is used to validate the wing deformations predicted by finite element method (FEA).

Original language	English
Title of host publication	Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics
Editors	Raman Singh, Raman Singh, Geoffrey Slipher
Publisher	Springer
Pages	101-104
Number of pages	4
ISBN (Print)	9783030300272
DOIs	https://doi.org/10.1007/978-3-030-30028-9_16
State	Published - 2020
Externally published	Yes
Event	SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2019 - Reno, United States Duration: Jun 3 2019 → Jun 6 2019

Publication series

Name	Conference Proceedings of the Society for Experimental Mechanics Series
ISSN (Print)	2191-5644
ISSN (Electronic)	2191-5652

Conference

Conference	SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2019
Country/Territory	United States
City	Reno
Period	06/3/19 → 06/6/19

Funding

The authors would like to thank the STTR program under the Air Force Office of Scientific Research for the funding.

Funders	Funder number
Air Force Office of Scientific Research

Keywords

Digital image correlation
Finite element analysis
Macro fiber composites
Morphing

Access to Document

10.1007/978-3-030-30028-9_16

Cite this

Mennu, M. M., Tran, B., Ifju, P. G., & Santamaria, E. (2020). Full-Field Deformation Measurement of Morphing Wings. In R. Singh, R. Singh, & G. Slipher (Eds.), Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics (pp. 101-104). (Conference Proceedings of the Society for Experimental Mechanics Series). Springer. https://doi.org/10.1007/978-3-030-30028-9_16

Mennu, M. M. ; Tran, B. ; Ifju, P. G. et al. / Full-Field Deformation Measurement of Morphing Wings. Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics. editor / Raman Singh ; Raman Singh ; Geoffrey Slipher. Springer, 2020. pp. 101-104 (Conference Proceedings of the Society for Experimental Mechanics Series).

@inproceedings{3759ac59e12b4d8fbee04877cd06e3ec,

title = "Full-Field Deformation Measurement of Morphing Wings",

abstract = "A micro air vehicle that can achieve a versatile flight condition is being designed. One way of achieving such versatility is through biomimicry. One aspect of this design utilizes a bird-like wing that changes shape to match four flight regimes; take-off-and -landing, cruise, high speed dash and one that enhances maneuverability. A joint mechanism using a tendon actuator between the inboard and the outboard portions of the wing is used to modify wing sweep. Macro fiber composites (MFCs) piezoelectric actuators in a bi-morph configuration are incorporated into the MAVs as control mechanism. Camber changes are implemented with tendon actuators. Finite element is used to model the wing section and perform a full-field deformation study and compared with experimental results. Digital image correlation is used to validate the wing deformations predicted by finite element method (FEA).",

keywords = "Digital image correlation, Finite element analysis, Macro fiber composites, Morphing",

author = "Mennu, {M. M.} and B. Tran and Ifju, {P. G.} and E. Santamaria",

note = "Publisher Copyright: {\textcopyright} Society for Experimental Mechanics, Inc. 2020.; SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2019 ; Conference date: 03-06-2019 Through 06-06-2019",

year = "2020",

doi = "10.1007/978-3-030-30028-9_16",

language = "English",

isbn = "9783030300272",

series = "Conference Proceedings of the Society for Experimental Mechanics Series",

publisher = "Springer",

pages = "101--104",

editor = "Raman Singh and Raman Singh and Geoffrey Slipher",

booktitle = "Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics",

}

Mennu, MM, Tran, B, Ifju, PG & Santamaria, E 2020, Full-Field Deformation Measurement of Morphing Wings. in R Singh, R Singh & G Slipher (eds), Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics. Conference Proceedings of the Society for Experimental Mechanics Series, Springer, pp. 101-104, SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2019, Reno, United States, 06/3/19. https://doi.org/10.1007/978-3-030-30028-9_16

Full-Field Deformation Measurement of Morphing Wings. / Mennu, M. M.; Tran, B.; Ifju, P. G. et al.
Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics. ed. / Raman Singh; Raman Singh; Geoffrey Slipher. Springer, 2020. p. 101-104 (Conference Proceedings of the Society for Experimental Mechanics Series).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Full-Field Deformation Measurement of Morphing Wings

AU - Mennu, M. M.

AU - Tran, B.

AU - Ifju, P. G.

AU - Santamaria, E.

N1 - Publisher Copyright: © Society for Experimental Mechanics, Inc. 2020.

PY - 2020

Y1 - 2020

N2 - A micro air vehicle that can achieve a versatile flight condition is being designed. One way of achieving such versatility is through biomimicry. One aspect of this design utilizes a bird-like wing that changes shape to match four flight regimes; take-off-and -landing, cruise, high speed dash and one that enhances maneuverability. A joint mechanism using a tendon actuator between the inboard and the outboard portions of the wing is used to modify wing sweep. Macro fiber composites (MFCs) piezoelectric actuators in a bi-morph configuration are incorporated into the MAVs as control mechanism. Camber changes are implemented with tendon actuators. Finite element is used to model the wing section and perform a full-field deformation study and compared with experimental results. Digital image correlation is used to validate the wing deformations predicted by finite element method (FEA).

AB - A micro air vehicle that can achieve a versatile flight condition is being designed. One way of achieving such versatility is through biomimicry. One aspect of this design utilizes a bird-like wing that changes shape to match four flight regimes; take-off-and -landing, cruise, high speed dash and one that enhances maneuverability. A joint mechanism using a tendon actuator between the inboard and the outboard portions of the wing is used to modify wing sweep. Macro fiber composites (MFCs) piezoelectric actuators in a bi-morph configuration are incorporated into the MAVs as control mechanism. Camber changes are implemented with tendon actuators. Finite element is used to model the wing section and perform a full-field deformation study and compared with experimental results. Digital image correlation is used to validate the wing deformations predicted by finite element method (FEA).

KW - Digital image correlation

KW - Finite element analysis

KW - Macro fiber composites

KW - Morphing

UR - http://www.scopus.com/inward/record.url?scp=85085487201&partnerID=8YFLogxK

U2 - 10.1007/978-3-030-30028-9_16

DO - 10.1007/978-3-030-30028-9_16

M3 - Conference contribution

AN - SCOPUS:85085487201

SN - 9783030300272

T3 - Conference Proceedings of the Society for Experimental Mechanics Series

SP - 101

EP - 104

BT - Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics

A2 - Singh, Raman

A2 - Slipher, Geoffrey

PB - Springer

T2 - SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2019

Y2 - 3 June 2019 through 6 June 2019

ER -

Mennu MM, Tran B, Ifju PG, Santamaria E. Full-Field Deformation Measurement of Morphing Wings. In Singh R, Singh R, Slipher G, editors, Mechanics of Composite and Multi-functional Materials, Volume 5 - Proceedings of the 2019 Annual Conference on Experimental and Applied Mechanics. Springer. 2020. p. 101-104. (Conference Proceedings of the Society for Experimental Mechanics Series). doi: 10.1007/978-3-030-30028-9_16

Full-Field Deformation Measurement of Morphing Wings

Abstract

Publication series

Conference

Funding

Keywords

Access to Document

Other files and links

Fingerprint

Cite this