Conceptual Design of an Airfoil with Temperature-Responsive Polymer
The accelerated growth in aircraft industries desire
effectual schemes, programs, innovative designs of advanced systems
and facilities to accomplish the augmenting need for home-free air
transportation. In this paper, a contemporary conceptual design of a
cambered airfoil has been proposed in order to providing augmented
effective lift force relative to the airplane, and to eliminating
drawbacks and limitations of an airfoil in a commercial airplane by
using a kind of smart materials. This invention of an unsymmetrical
airfoil structure utilizes the amplified air momentum around the
airfoil and increased camber length to providing improved aircraft
performance and assist to enhancing the reliability of the aircraft
components. Moreover, this conjectured design helps to reducing
airplane weight and total drag.
<p>[1] B. Culshaw. Smart Structures & Materials. Artech House, 1996.
[2] M. V. Gandhi & B. S. Thompson. Smart Materials and Structures.
Chapman & Hall 1992.
[3] Abdelber Bendaoud, Marius Plopeanu, Karim Medles, Amar Tilmanite
Lucien Dascalescu, “Experimental study of corona discharge generated
by a triode electrode system”,Proc. 2012 Joint Electrostatics
Conference, CNRS - University of Poitiers-ENSMA IUT,Angouleme
16021, France.
[4] Omar Abdel Razek, Sherif Fahmy, Farid Abdel-Kader,Mostafa Ehsan,
“Nano manufacturing and Smart Materials”, MENG 439,Advanced
Manufacturing Processes.
[5] Dr. K. Muthumani, Dr. R. Sreekala, “Structural Application of Smart
Materials”, Structural Engineering Research Centre, Chennai.
[6] C. S. Cai, Wenjie Wu, Suren Chen, George Voyiadjis, “Applications of
Smart Materials in Structural Engineering”, LTRC Project No. 02-
4TIRE, State Project No. 736-99-1055, Department of Civil
Engineering, Louisiana State University, Baton Rouge, Louisiana 70803,
2003.
[7] Anupam Tiwari, “Smart materials for military applications”, National
conference on Emerging trends in Intelligent computing and
communication, Galgotias college of engineering & Technology,
Greater Noida.
[8] Smart materials used in medical applications.
[9] A. Bendaoud, A.Tilmatine, K. Medles, O. Blejan, L. Dascalescu,
Experimental study of corona discharge generated in a modified wire
plate electrode configuration for electrostatic processes applications,
IEEE, Trans. Ind. Appl., 46 (2010) 666-671
[10] Arman Molkioung, “Simple Demonstration of the Seebeck Effect”,
Science Education Review, 9(3), 2010.
[11] Darold B. Cummings, Aaron J. Kutzmann, Christopher K. Droney,
“Aircraft with thrust vectoring for switchably providing upper surface
blowing”, US Patent no. 6926229 B2
[12] I.A. Krichtafovitch, V.L. Gorobets, S.V. Karpov, and A.V. Mamishev
“Electrostatic Fluid Accelerator and Air Purifier-The Second Wind”,
Kronos Air Technologies, 8551 154th Ave NE, Redmond, WA 98052.</p>
<p>[1] B. Culshaw. Smart Structures & Materials. Artech House, 1996.
[2] M. V. Gandhi & B. S. Thompson. Smart Materials and Structures.
Chapman & Hall 1992.
[3] Abdelber Bendaoud, Marius Plopeanu, Karim Medles, Amar Tilmanite
Lucien Dascalescu, “Experimental study of corona discharge generated
by a triode electrode system”,Proc. 2012 Joint Electrostatics
Conference, CNRS - University of Poitiers-ENSMA IUT,Angouleme
16021, France.
[4] Omar Abdel Razek, Sherif Fahmy, Farid Abdel-Kader,Mostafa Ehsan,
“Nano manufacturing and Smart Materials”, MENG 439,Advanced
Manufacturing Processes.
[5] Dr. K. Muthumani, Dr. R. Sreekala, “Structural Application of Smart
Materials”, Structural Engineering Research Centre, Chennai.
[6] C. S. Cai, Wenjie Wu, Suren Chen, George Voyiadjis, “Applications of
Smart Materials in Structural Engineering”, LTRC Project No. 02-
4TIRE, State Project No. 736-99-1055, Department of Civil
Engineering, Louisiana State University, Baton Rouge, Louisiana 70803,
2003.
[7] Anupam Tiwari, “Smart materials for military applications”, National
conference on Emerging trends in Intelligent computing and
communication, Galgotias college of engineering & Technology,
Greater Noida.
[8] Smart materials used in medical applications.
[9] A. Bendaoud, A.Tilmatine, K. Medles, O. Blejan, L. Dascalescu,
Experimental study of corona discharge generated in a modified wire
plate electrode configuration for electrostatic processes applications,
IEEE, Trans. Ind. Appl., 46 (2010) 666-671
[10] Arman Molkioung, “Simple Demonstration of the Seebeck Effect”,
Science Education Review, 9(3), 2010.
[11] Darold B. Cummings, Aaron J. Kutzmann, Christopher K. Droney,
“Aircraft with thrust vectoring for switchably providing upper surface
blowing”, US Patent no. 6926229 B2
[12] I.A. Krichtafovitch, V.L. Gorobets, S.V. Karpov, and A.V. Mamishev
“Electrostatic Fluid Accelerator and Air Purifier-The Second Wind”,
Kronos Air Technologies, 8551 154th Ave NE, Redmond, WA 98052.</p>
@article{"International Journal of Mechanical, Industrial and Aerospace Sciences:58574", author = "Mohammed Niyasdeen Nejaamtheen", title = "Conceptual Design of an Airfoil with Temperature-Responsive Polymer", abstract = "The accelerated growth in aircraft industries desire
effectual schemes, programs, innovative designs of advanced systems
and facilities to accomplish the augmenting need for home-free air
transportation. In this paper, a contemporary conceptual design of a
cambered airfoil has been proposed in order to providing augmented
effective lift force relative to the airplane, and to eliminating
drawbacks and limitations of an airfoil in a commercial airplane by
using a kind of smart materials. This invention of an unsymmetrical
airfoil structure utilizes the amplified air momentum around the
airfoil and increased camber length to providing improved aircraft
performance and assist to enhancing the reliability of the aircraft
components. Moreover, this conjectured design helps to reducing
airplane weight and total drag.
", keywords = "Collector electrode, corona electrode, Temperatureresponsive
polymer and ultra-faims microchip.", volume = "7", number = "7", pages = "1599-3", }
