Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil

In the design of a morphing wing mechanism, actuation costs need to be taken into consideration. The energy required for the morphing can be reduced or increased depending on the nature of the morphing and also the speed at which the morphing occurs. A theoretical actuation cost model was develo...

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Main Author: Chan, Adil Arif.
Other Authors: Jorg Uwe Schluter
Format: Final Year Project
Language:English
Published: 2010
Subjects:
Online Access:http://hdl.handle.net/10356/40456
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-404562023-03-04T18:34:24Z Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil Chan, Adil Arif. Jorg Uwe Schluter School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics In the design of a morphing wing mechanism, actuation costs need to be taken into consideration. The energy required for the morphing can be reduced or increased depending on the nature of the morphing and also the speed at which the morphing occurs. A theoretical actuation cost model was developed to provide an estimate for the forces required for a particular flight configuration in the transonic regime. Transonic airfoils RAE 5213 and RAE 5215 were considered for the morphing and validations of prior wind tunnel test results from research journals was done by comparing with flow simulation results from FLUENT. Simulations were done for three angle of attacks of 0.350, 0.850 and 1.350, and at Mach number between 0.60 and 0.85. Simulation results showed similar trends to the experimental results, however at a higher magnitude. A mechanism for the morphing wing was designed for future manufacture and wind tunnel testing. Dimensions were considered carefully based on the wind tunnel facility in NTU. However, due to the limitations of NTU’s wind tunnel facility, which could run only at a maximum speed of 90m/s (Mach 0.30), the transonic morphing wing, could not be tested. The theoretical actuation costs were calculated for Mach 0.80 at an angle of attack of 0.850. Results showed that the strong aerodynamic force due to the high flow speed causes an upward camber detrimental to the airfoil morphing. Bachelor of Engineering (Aerospace Engineering) 2010-06-16T00:53:25Z 2010-06-16T00:53:25Z 2010 2010 Final Year Project (FYP) http://hdl.handle.net/10356/40456 en Nanyang Technological University 73 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Chan, Adil Arif.
Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
description In the design of a morphing wing mechanism, actuation costs need to be taken into consideration. The energy required for the morphing can be reduced or increased depending on the nature of the morphing and also the speed at which the morphing occurs. A theoretical actuation cost model was developed to provide an estimate for the forces required for a particular flight configuration in the transonic regime. Transonic airfoils RAE 5213 and RAE 5215 were considered for the morphing and validations of prior wind tunnel test results from research journals was done by comparing with flow simulation results from FLUENT. Simulations were done for three angle of attacks of 0.350, 0.850 and 1.350, and at Mach number between 0.60 and 0.85. Simulation results showed similar trends to the experimental results, however at a higher magnitude. A mechanism for the morphing wing was designed for future manufacture and wind tunnel testing. Dimensions were considered carefully based on the wind tunnel facility in NTU. However, due to the limitations of NTU’s wind tunnel facility, which could run only at a maximum speed of 90m/s (Mach 0.30), the transonic morphing wing, could not be tested. The theoretical actuation costs were calculated for Mach 0.80 at an angle of attack of 0.850. Results showed that the strong aerodynamic force due to the high flow speed causes an upward camber detrimental to the airfoil morphing.
author2 Jorg Uwe Schluter
author_facet Jorg Uwe Schluter
Chan, Adil Arif.
format Final Year Project
author Chan, Adil Arif.
author_sort Chan, Adil Arif.
title Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
title_short Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
title_full Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
title_fullStr Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
title_full_unstemmed Aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
title_sort aerodynamics of unconventional airfoils - actuation force of variable cambered airfoil
publishDate 2010
url http://hdl.handle.net/10356/40456
_version_ 1759856051605209088