Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel

Thi Tuyet Nhung Le; Thanh Phat Duong; Nhat Truong Hoang

doi:doi:10.11648/j.ijtet.s.2016020501.12

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Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel

Thi Tuyet Nhung Le, Thanh Phat Duong, Nhat Truong Hoang

Published in International Journal of Transportation Engineering and Technology (Volume 2, Issue 4-1)

Received: 16 August 2016 Accepted: 22 August 2016 Published: 19 September 2016

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Abstract

The purpose of this study is to take measures to manufacture the experimental model: NACA 0012 wing model in the low speed wind tunnel (38 m/s). The parameters base on the achieved results of Thi-Tuyet Nhung Le & al.: “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing’s parameters on flutter speed”. As flutter is a destructive phenomenon, many studies has researched and manufactured experimental models. The suitable material of wing is polyurethane elastomer. The suitable method which manufactures the wing model is CNC method.

Published in	International Journal of Transportation Engineering and Technology (Volume 2, Issue 4-1) This article belongs to the Special Issue Experiments Researches in Aeronautical Engineering
DOI	10.11648/j.ijtet.s.2016020501.12
Page(s)	7-11
Creative Commons	This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.
Copyright	Copyright © The Author(s), 2016. Published by Science Publishing Group

Keywords

Methods of Manufacturing, Aeroelasticity, Bench Test for NACA0012

References

[1]	Guertin, Master thesis “The Applycation of Finite Element Method to Aeroelastic Lifting Surface Flutter”, Rice University, Houston, April 2012.
[2]	Ashley H., Zartarian G., “Piston Theory – A New Aerodynamic Tool for the Aeroelastician”, Twenty-Fourth Annual Meeting, IAS, New York, January 23-26, 1956.
[3]	Smilg, В. and L. S. Wasserman, “Application of Three-Dimensional Flutter Theory to Aircraft Structures”, U.S. Army Air Force Tech. Rept. 4798, 1942.
[4]	H. N. Vang “Phân tích ảnh hưởng của các thông số hình học đến hiện tượng bất ổn định về khí động đàn hồi của cánh NACA 0012 trong hầm gió vận tốc thấp”, Eng. thesis, Univ. of Technology, Ho Chi Minh, Viet Nam, 2015.
[5]	T. A. NGUYEN, H. N. VANG, Viet Khai NGUYEN, Thi Tuyet Nhung LE, Chi Cong NGUYEN, “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel”, Journal of Transportation Science and Technolog, Vol. 7+8, pp. 163-169, 2013.
[6]	Roberto Gil Annes da Silva, “Aeroservoelastic modeling of a flexible wing for wind tunnel flutter test”, 20th International Congress of Mechanical Engineering, Gramado, RS, Brazil, November 15-20, 2009.
[7]	M. Kassem Abbas, Hany M Negm, M Adnan Elshafei, “Flutter and Divergence Characteristics of Composite Plate Wing”, International Journal of Engineering and Innovative Technology (IJEIT) Vol. 4, Issue. 2, August 2014.
[8]	Ahmet Aran, course “Manufacturing properties of engineering materials, Işık University, Turkey, pp. 52-64, 2007.
[9]	Colton, “Failure of rapid prototype molds during injection molding”, Georgia Institute of Technology, USA. CIRP Annals-Manufacturing Technology, Issue 1, pp. 129-132, December 31, 2001.
[10]	Thanh Phat Duong, Nhat Truong Hoang, “Methods of manufacturing aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel”, 6th Scientific Research Conference of PFIEV – HCMUT Students, Ho Chi Minh City Univ. of Technology, Viet Nam, 2016.

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APA Style

Thi Tuyet Nhung Le, Thanh Phat Duong, Nhat Truong Hoang. (2016). Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel. International Journal of Transportation Engineering and Technology, 2(4-1), 7-11. https://doi.org/10.11648/j.ijtet.s.2016020501.12

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ACS Style

Thi Tuyet Nhung Le; Thanh Phat Duong; Nhat Truong Hoang. Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel. Int. J. Transp. Eng. Technol. 2016, 2(4-1), 7-11. doi: 10.11648/j.ijtet.s.2016020501.12

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AMA Style

Thi Tuyet Nhung Le, Thanh Phat Duong, Nhat Truong Hoang. Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel. Int J Transp Eng Technol. 2016;2(4-1):7-11. doi: 10.11648/j.ijtet.s.2016020501.12

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@article{10.11648/j.ijtet.s.2016020501.12,
  author = {Thi Tuyet Nhung Le and Thanh Phat Duong and Nhat Truong Hoang},
  title = {Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel},
  journal = {International Journal of Transportation Engineering and Technology},
  volume = {2},
  number = {4-1},
  pages = {7-11},
  doi = {10.11648/j.ijtet.s.2016020501.12},
  url = {https://doi.org/10.11648/j.ijtet.s.2016020501.12},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ijtet.s.2016020501.12},
  abstract = {The purpose of this study is to take measures to manufacture the experimental model: NACA 0012 wing model in the low speed wind tunnel (38 m/s). The parameters base on the achieved results of Thi-Tuyet Nhung Le & al.: “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing’s parameters on flutter speed”. As flutter is a destructive phenomenon, many studies has researched and manufactured experimental models. The suitable material of wing is polyurethane elastomer. The suitable method which manufactures the wing model is CNC method.},
 year = {2016}
}

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TY  - JOUR
T1  - Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel
AU  - Thi Tuyet Nhung Le
AU  - Thanh Phat Duong
AU  - Nhat Truong Hoang
Y1  - 2016/09/19
PY  - 2016
N1  - https://doi.org/10.11648/j.ijtet.s.2016020501.12
DO  - 10.11648/j.ijtet.s.2016020501.12
T2  - International Journal of Transportation Engineering and Technology
JF  - International Journal of Transportation Engineering and Technology
JO  - International Journal of Transportation Engineering and Technology
SP  - 7
EP  - 11
PB  - Science Publishing Group
SN  - 2575-1751
UR  - https://doi.org/10.11648/j.ijtet.s.2016020501.12
AB  - The purpose of this study is to take measures to manufacture the experimental model: NACA 0012 wing model in the low speed wind tunnel (38 m/s). The parameters base on the achieved results of Thi-Tuyet Nhung Le & al.: “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing’s parameters on flutter speed”. As flutter is a destructive phenomenon, many studies has researched and manufactured experimental models. The suitable material of wing is polyurethane elastomer. The suitable method which manufactures the wing model is CNC method.
VL  - 2
IS  - 4-1
ER  -

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Author Information

Thi Tuyet Nhung Le

Department of Aeronautical & Space Engineering, School of Transportation Engineering, Hanoi University of Science and Technology, Hanoi, Vietnam
Thanh Phat Duong

Department. of Aerospace Engineering, Faculty of Transport Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam
Nhat Truong Hoang

Department. of Aerospace Engineering, Faculty of Transport Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam

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Plain Text BibTeX RIS

APA Style

Thi Tuyet Nhung Le, Thanh Phat Duong, Nhat Truong Hoang. (2016). Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel. International Journal of Transportation Engineering and Technology, 2(4-1), 7-11. https://doi.org/10.11648/j.ijtet.s.2016020501.12

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ACS Style

Thi Tuyet Nhung Le; Thanh Phat Duong; Nhat Truong Hoang. Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel. Int. J. Transp. Eng. Technol. 2016, 2(4-1), 7-11. doi: 10.11648/j.ijtet.s.2016020501.12

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AMA Style

Thi Tuyet Nhung Le, Thanh Phat Duong, Nhat Truong Hoang. Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel. Int J Transp Eng Technol. 2016;2(4-1):7-11. doi: 10.11648/j.ijtet.s.2016020501.12

Copy | Download

@article{10.11648/j.ijtet.s.2016020501.12,
  author = {Thi Tuyet Nhung Le and Thanh Phat Duong and Nhat Truong Hoang},
  title = {Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel},
  journal = {International Journal of Transportation Engineering and Technology},
  volume = {2},
  number = {4-1},
  pages = {7-11},
  doi = {10.11648/j.ijtet.s.2016020501.12},
  url = {https://doi.org/10.11648/j.ijtet.s.2016020501.12},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ijtet.s.2016020501.12},
  abstract = {The purpose of this study is to take measures to manufacture the experimental model: NACA 0012 wing model in the low speed wind tunnel (38 m/s). The parameters base on the achieved results of Thi-Tuyet Nhung Le & al.: “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing’s parameters on flutter speed”. As flutter is a destructive phenomenon, many studies has researched and manufactured experimental models. The suitable material of wing is polyurethane elastomer. The suitable method which manufactures the wing model is CNC method.},
 year = {2016}
}

Copy | Download

TY  - JOUR
T1  - Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel
AU  - Thi Tuyet Nhung Le
AU  - Thanh Phat Duong
AU  - Nhat Truong Hoang
Y1  - 2016/09/19
PY  - 2016
N1  - https://doi.org/10.11648/j.ijtet.s.2016020501.12
DO  - 10.11648/j.ijtet.s.2016020501.12
T2  - International Journal of Transportation Engineering and Technology
JF  - International Journal of Transportation Engineering and Technology
JO  - International Journal of Transportation Engineering and Technology
SP  - 7
EP  - 11
PB  - Science Publishing Group
SN  - 2575-1751
UR  - https://doi.org/10.11648/j.ijtet.s.2016020501.12
AB  - The purpose of this study is to take measures to manufacture the experimental model: NACA 0012 wing model in the low speed wind tunnel (38 m/s). The parameters base on the achieved results of Thi-Tuyet Nhung Le & al.: “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing’s parameters on flutter speed”. As flutter is a destructive phenomenon, many studies has researched and manufactured experimental models. The suitable material of wing is polyurethane elastomer. The suitable method which manufactures the wing model is CNC method.
VL  - 2
IS  - 4-1
ER  -

Copy | Download