Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude

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DU, Sha ;ANG, Haisong .
Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 58, n.1, p. 46-55, june 2018. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/sl/article/design-and-feasibility-analyses-of-morphing-airfoil-used-to-control-flight-attitude/>. Date accessed: 24 aug. 2019. 
doi:http://dx.doi.org/10.5545/sv-jme.2011.189.
Du, S., & Ang, H.
(2012).
Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude.
Strojniški vestnik - Journal of Mechanical Engineering, 58(1), 46-55.
doi:http://dx.doi.org/10.5545/sv-jme.2011.189
@article{sv-jmesv-jme.2011.189,
	author = {Sha  Du and Haisong  Ang},
	title = {Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {58},
	number = {1},
	year = {2012},
	keywords = {morphing wing; deformation institutions; traditional control surface; aerodynamic character; optimal design; compare},
	abstract = {Morphing technology, inspired by bat and bird flight can enable an aircraft to adapt its shape to enhance mission performance and optimize flight attitude controlling efficiency. A morphing airfoil concept is proposed to replace the traditional flap, ailerons, elevator and rudders in order to improve aerodynamic efficiency in this paper. A procedure is used to virtually simulate a morphing wing to perform fast, relatively accurately and efficiently. A set of optimal airfoil shapes obtained are aimed at minimizing the aerodynamic drag character by optimizing morphing configurations at different Cl under the twodimensional steady-flow simulation. These airfoil shapes are used to maneuver flight attitude, minimize drag and take place of traditional control surfaces of different rolling, yawing and pitching moment. Then, the basic relationships between optimized morphing airfoil and the traditional control element on rolling, pitching and yawing moment are simplified to the relationship of Cl. The morphing airfoil shapes at different Cl are represented. The configuration of traditional airfoil and morphing airfoil at different Cl are compared. It is proved that morphing wing can be used to take the place of a traditional wing.},
	issn = {0039-2480},	pages = {46-55},	doi = {10.5545/sv-jme.2011.189},
	url = {https://www.sv-jme.eu/sl/article/design-and-feasibility-analyses-of-morphing-airfoil-used-to-control-flight-attitude/}
}
Du, S.,Ang, H.
2012 June 58. Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 58:1
%A Du, Sha 
%A Ang, Haisong 
%D 2012
%T Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude
%B 2012
%9 morphing wing; deformation institutions; traditional control surface; aerodynamic character; optimal design; compare
%! Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude
%K morphing wing; deformation institutions; traditional control surface; aerodynamic character; optimal design; compare
%X Morphing technology, inspired by bat and bird flight can enable an aircraft to adapt its shape to enhance mission performance and optimize flight attitude controlling efficiency. A morphing airfoil concept is proposed to replace the traditional flap, ailerons, elevator and rudders in order to improve aerodynamic efficiency in this paper. A procedure is used to virtually simulate a morphing wing to perform fast, relatively accurately and efficiently. A set of optimal airfoil shapes obtained are aimed at minimizing the aerodynamic drag character by optimizing morphing configurations at different Cl under the twodimensional steady-flow simulation. These airfoil shapes are used to maneuver flight attitude, minimize drag and take place of traditional control surfaces of different rolling, yawing and pitching moment. Then, the basic relationships between optimized morphing airfoil and the traditional control element on rolling, pitching and yawing moment are simplified to the relationship of Cl. The morphing airfoil shapes at different Cl are represented. The configuration of traditional airfoil and morphing airfoil at different Cl are compared. It is proved that morphing wing can be used to take the place of a traditional wing.
%U https://www.sv-jme.eu/sl/article/design-and-feasibility-analyses-of-morphing-airfoil-used-to-control-flight-attitude/
%0 Journal Article
%R 10.5545/sv-jme.2011.189
%& 46
%P 10
%J Strojniški vestnik - Journal of Mechanical Engineering
%V 58
%N 1
%@ 0039-2480
%8 2018-06-28
%7 2018-06-28
Du, Sha, & Haisong  Ang.
"Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude." Strojniški vestnik - Journal of Mechanical Engineering [Online], 58.1 (2012): 46-55. Web.  24 Aug. 2019
TY  - JOUR
AU  - Du, Sha 
AU  - Ang, Haisong 
PY  - 2012
TI  - Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 10.5545/sv-jme.2011.189
KW  - morphing wing; deformation institutions; traditional control surface; aerodynamic character; optimal design; compare
N2  - Morphing technology, inspired by bat and bird flight can enable an aircraft to adapt its shape to enhance mission performance and optimize flight attitude controlling efficiency. A morphing airfoil concept is proposed to replace the traditional flap, ailerons, elevator and rudders in order to improve aerodynamic efficiency in this paper. A procedure is used to virtually simulate a morphing wing to perform fast, relatively accurately and efficiently. A set of optimal airfoil shapes obtained are aimed at minimizing the aerodynamic drag character by optimizing morphing configurations at different Cl under the twodimensional steady-flow simulation. These airfoil shapes are used to maneuver flight attitude, minimize drag and take place of traditional control surfaces of different rolling, yawing and pitching moment. Then, the basic relationships between optimized morphing airfoil and the traditional control element on rolling, pitching and yawing moment are simplified to the relationship of Cl. The morphing airfoil shapes at different Cl are represented. The configuration of traditional airfoil and morphing airfoil at different Cl are compared. It is proved that morphing wing can be used to take the place of a traditional wing.
UR  - https://www.sv-jme.eu/sl/article/design-and-feasibility-analyses-of-morphing-airfoil-used-to-control-flight-attitude/
@article{{sv-jme}{sv-jme.2011.189},
	author = {Du, S., Ang, H.},
	title = {Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {58},
	number = {1},
	year = {2012},
	doi = {10.5545/sv-jme.2011.189},
	url = {https://www.sv-jme.eu/sl/article/design-and-feasibility-analyses-of-morphing-airfoil-used-to-control-flight-attitude/}
}
TY  - JOUR
AU  - Du, Sha 
AU  - Ang, Haisong 
PY  - 2018/06/28
TI  - Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 58, No 1 (2012): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 10.5545/sv-jme.2011.189
KW  - morphing wing, deformation institutions, traditional control surface, aerodynamic character, optimal design, compare
N2  - Morphing technology, inspired by bat and bird flight can enable an aircraft to adapt its shape to enhance mission performance and optimize flight attitude controlling efficiency. A morphing airfoil concept is proposed to replace the traditional flap, ailerons, elevator and rudders in order to improve aerodynamic efficiency in this paper. A procedure is used to virtually simulate a morphing wing to perform fast, relatively accurately and efficiently. A set of optimal airfoil shapes obtained are aimed at minimizing the aerodynamic drag character by optimizing morphing configurations at different Cl under the twodimensional steady-flow simulation. These airfoil shapes are used to maneuver flight attitude, minimize drag and take place of traditional control surfaces of different rolling, yawing and pitching moment. Then, the basic relationships between optimized morphing airfoil and the traditional control element on rolling, pitching and yawing moment are simplified to the relationship of Cl. The morphing airfoil shapes at different Cl are represented. The configuration of traditional airfoil and morphing airfoil at different Cl are compared. It is proved that morphing wing can be used to take the place of a traditional wing.
UR  - https://www.sv-jme.eu/sl/article/design-and-feasibility-analyses-of-morphing-airfoil-used-to-control-flight-attitude/
Du, Sha, AND Ang, Haisong.
"Design and Feasibility Analyses of Morphing Airfoil Used to Control Flight Attitude" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 58 Number 1 (28 June 2018)

Avtorji

Inštitucije

  • College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, China
  • College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, China

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 58(2012)1, 46-55

10.5545/sv-jme.2011.189

Morphing technology, inspired by bat and bird flight can enable an aircraft to adapt its shape to enhance mission performance and optimize flight attitude controlling efficiency. A morphing airfoil concept is proposed to replace the traditional flap, ailerons, elevator and rudders in order to improve aerodynamic efficiency in this paper. A procedure is used to virtually simulate a morphing wing to perform fast, relatively accurately and efficiently. A set of optimal airfoil shapes obtained are aimed at minimizing the aerodynamic drag character by optimizing morphing configurations at different Cl under the twodimensional steady-flow simulation. These airfoil shapes are used to maneuver flight attitude, minimize drag and take place of traditional control surfaces of different rolling, yawing and pitching moment. Then, the basic relationships between optimized morphing airfoil and the traditional control element on rolling, pitching and yawing moment are simplified to the relationship of Cl. The morphing airfoil shapes at different Cl are represented. The configuration of traditional airfoil and morphing airfoil at different Cl are compared. It is proved that morphing wing can be used to take the place of a traditional wing.

morphing wing; deformation institutions; traditional control surface; aerodynamic character; optimal design; compare