Grant: Discovery Grants Program - Individual
Royal Military College of Canada
$32,000.00
Characterization, Optimization and Application of Leading-Edge Tubercle Wings
EF 2018-19
Résumé
Leading-edge tubercles are aerodynamic devices biologically inspired from the morphology of hump-back whale fins. In the case of whales, the fin tubercles appear to be a functional adaptation which allow it to enhance turning maneuverability during prey capture. For conventional wings, tubercles on the leading-edge act as passive flow-control devices. Initial empirical evidence has shown potential benefits of tubercle leading-edge wings to delay stall and improve post-stall characteristics. The shape and placement of the tubercles along a wing leading edge, expressed in terms of tubercle wavelength and amplitude, seem to play a critical role on its aerodynamic performance. To date however, significant challenges worthy of further study remain in understanding the sensitivity of tubercle shape and placement parameters to the flow of finite span wings in the subsonic to transonic flow regimes and in the design and application of this bioinspired devices. The project aims to gain additional knowledge on the fluid dynamics behaviour of leading edge tubercles through wind-tunnel testing and flow visualization. It also aims to develop analysis and design approaches to optimize the shape of this devices and explore their potential applications. In particular, the project will explore potential gains of applying tubercles to enhanced low speed, high angle of attack and turning performance for unmanned aerial vehicles as well as mitigate large induced angle of attack and dynamic stall interactions for vertical axis wind-turbines which can improve their energy extractions. Moreover the project will provide training for students in the areas of experimental and computational fluid mechanics, applied aerodynamics, design synthesis and numerical optimization.
Programme
Discovery Grants Program - Individual
Bénéficiaire
Emplacement
Ontario, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
RGPIN-2018-04374
Name nom
Perez, Ruben
Department département
Mechanical Engineering
Organization id
30
Institution établissement
Royal Military College of Canada
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2018
Competition year année de concours
2018
Award amount
32000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
Discovery grants programs
Group fr
Programmes de subventions à la découverte
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2108
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Aerospace, aeronautical and automotive engineering
Research subject fr
Génie aérospatial, aéronautique et automobile
Partie
1
Nb partie
5
Application title
Characterization, Optimization and Application of Leading-Edge Tubercle Wings
Keyword
NSERC
Application summary
Leading-edge tubercles are aerodynamic devices biologically inspired from the morphology of hump-back whale fins. In the case of whales, the fin tubercles appear to be a functional adaptation which allow it to enhance turning maneuverability during prey capture. For conventional wings, tubercles on the leading-edge act as passive flow-control devices. Initial empirical evidence has shown potential benefits of tubercle leading-edge wings to delay stall and improve post-stall characteristics. The shape and placement of the tubercles along a wing leading edge, expressed in terms of tubercle wavelength and amplitude, seem to play a critical role on its aerodynamic performance. To date however, significant challenges worthy of further study remain in understanding the sensitivity of tubercle shape and placement parameters to the flow of finite span wings in the subsonic to transonic flow regimes and in the design and application of this bioinspired devices. The project aims to gain additional knowledge on the fluid dynamics behaviour of leading edge tubercles through wind-tunnel testing and flow visualization. It also aims to develop analysis and design approaches to optimize the shape of this devices and explore their potential applications. In particular, the project will explore potential gains of applying tubercles to enhanced low speed, high angle of attack and turning performance for unmanned aerial vehicles as well as mitigate large induced angle of attack and dynamic stall interactions for vertical axis wind-turbines which can improve their energy extractions. Moreover the project will provide training for students in the areas of experimental and computational fluid mechanics, applied aerodynamics, design synthesis and numerical optimization.