Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures

Andres E Rivero; Jonathan E Cooper; Ben K S Woods

doi:10.2514/6.2020-1298

Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures

Andres E Rivero, Jonathan E Cooper, Ben K S Woods

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

6 Citations (Scopus)

456 Downloads (Pure)

Abstract

This paper presents a newly developed three-dimensional Fluid-Structure Interaction (FSI) routine for the Fish Bone Active Camber (FishBAC) concept that couples a three-dimensional Lifting-Line theory analysis to a two-dimensional viscous corrected panel method (XFOIL) to create a viscous corrected three-dimensional wing aerodynamic solver. This aerodynamic model is then coupled to a previously developed multi-component Mindlin-Reissner plate model based composite analysis routine for the FishBAC morphing device. The methodology is explained, and predictions are validated against existing modeling tools. The FSI model developed in this paper shows good agreement when compared gainst other structural, aerodynamic and FSI tools. Additionally, results show the FishBAC’s ability to improve aerodynamic performance at a wide range of operating conditions.

Original language	English
Title of host publication	AIAA Scitech 2020 Forum
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages	15
ISBN (Electronic)	978-1-62410-595-1
DOIs	https://doi.org/10.2514/6.2020-1298
Publication status	E-pub ahead of print - 5 Jan 2020
Event	AIAA SciTech Forum 2020 - Hyatt Regency Orlando, Orlando, United States Duration: 6 Jan 2020 → 10 Jan 2020

Conference

Conference	AIAA SciTech Forum 2020
Country/Territory	United States
City	Orlando
Period	6/01/20 → 10/01/20

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10.2514/6.2020-1298

Full-text PDF (accepted author manuscript)
This is the author accepted manuscript (AAM). The final published version (version of record) is available online via American Institute of Aeronautics and Astronautics at https://arc.aiaa.org/doi/abs/10.2514/6.2020-1298. Please refer to any applicable terms of use of the publisher.
Accepted author manuscript, 1.62 MB

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MDPI Aerospace Travel Award 2020
Rivero, A. E. (Recipient), 27 Jan 2020
Prize: Prizes, Medals, Awards and Grants
RAeS Aerospace Speakers Travel Grant (AeSTG)
Rivero, A. E. (Recipient), 31 Jan 2020
Prize: Prizes, Medals, Awards and Grants

Cite this

@inproceedings{24ec2765a4194ed28d5547f52ef0b466,

title = "Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures",

abstract = "This paper presents a newly developed three-dimensional Fluid-Structure Interaction (FSI) routine for the Fish Bone Active Camber (FishBAC) concept that couples a three-dimensional Lifting-Line theory analysis to a two-dimensional viscous corrected panel method (XFOIL) to create a viscous corrected three-dimensional wing aerodynamic solver. This aerodynamic model is then coupled to a previously developed multi-component Mindlin-Reissner plate model based composite analysis routine for the FishBAC morphing device. The methodology is explained, and predictions are validated against existing modeling tools. The FSI model developed in this paper shows good agreement when compared gainst other structural, aerodynamic and FSI tools. Additionally, results show the FishBAC{\textquoteright}s ability to improve aerodynamic performance at a wide range of operating conditions.",

author = "Rivero, {Andres E} and Cooper, {Jonathan E} and Woods, {Ben K S}",

year = "2020",

month = jan,

day = "5",

doi = "10.2514/6.2020-1298",

language = "English",

booktitle = "AIAA Scitech 2020 Forum",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

address = "United States",

note = "AIAA SciTech Forum 2020 ; Conference date: 06-01-2020 Through 10-01-2020",

}

Rivero, AE , Cooper, JE & Woods, BKS 2020, Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures. in AIAA Scitech 2020 Forum., 2020-1298, American Institute of Aeronautics and Astronautics Inc. (AIAA), AIAA SciTech Forum 2020, Orlando, Florida, United States, 6/01/20. https://doi.org/10.2514/6.2020-1298

Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures. / Rivero, Andres E ; Cooper, Jonathan E ; Woods, Ben K S.
AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2020. 2020-1298.

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

TY - GEN

T1 - Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures

AU - Rivero, Andres E

AU - Cooper, Jonathan E

AU - Woods, Ben K S

PY - 2020/1/5

Y1 - 2020/1/5

N2 - This paper presents a newly developed three-dimensional Fluid-Structure Interaction (FSI) routine for the Fish Bone Active Camber (FishBAC) concept that couples a three-dimensional Lifting-Line theory analysis to a two-dimensional viscous corrected panel method (XFOIL) to create a viscous corrected three-dimensional wing aerodynamic solver. This aerodynamic model is then coupled to a previously developed multi-component Mindlin-Reissner plate model based composite analysis routine for the FishBAC morphing device. The methodology is explained, and predictions are validated against existing modeling tools. The FSI model developed in this paper shows good agreement when compared gainst other structural, aerodynamic and FSI tools. Additionally, results show the FishBAC’s ability to improve aerodynamic performance at a wide range of operating conditions.

AB - This paper presents a newly developed three-dimensional Fluid-Structure Interaction (FSI) routine for the Fish Bone Active Camber (FishBAC) concept that couples a three-dimensional Lifting-Line theory analysis to a two-dimensional viscous corrected panel method (XFOIL) to create a viscous corrected three-dimensional wing aerodynamic solver. This aerodynamic model is then coupled to a previously developed multi-component Mindlin-Reissner plate model based composite analysis routine for the FishBAC morphing device. The methodology is explained, and predictions are validated against existing modeling tools. The FSI model developed in this paper shows good agreement when compared gainst other structural, aerodynamic and FSI tools. Additionally, results show the FishBAC’s ability to improve aerodynamic performance at a wide range of operating conditions.

U2 - 10.2514/6.2020-1298

DO - 10.2514/6.2020-1298

M3 - Conference Contribution (Conference Proceeding)

BT - AIAA Scitech 2020 Forum

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

T2 - AIAA SciTech Forum 2020

Y2 - 6 January 2020 through 10 January 2020

ER -

Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures

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Conference

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Prizes

MDPI Aerospace Travel Award 2020

RAeS Aerospace Speakers Travel Grant (AeSTG)

Cite this