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Grant: Collaborative Research and Development Grants

University of Victoria

$120,000.00

Multidisciplinary design optimization of novel aircaft configurations: stick-to-stress simulation, validation and evaluation (SAVANT)

FY 2014-15

Summary
The proposed research program aims to develop a comprehensive virtual multidisciplinary stick-to-stress design optimization framework for the synthesis of novel and energy efficient aircraft configurations. SAVANT proposes to combine flight dynamic models and nonlinear aeroelastic solvers based on aerodynamic reduced order models (ROM) to generate ""in real-time"" loads and stresses resulting from pilot input commands. Critical load identification methods and reduced order modelling techniques will potentially provide a step change in the efficiency and accuracy of the dynamic aeroelastic loads process. Identifying the flight conditions that lead to the maximum loads on aircraft structures and introducing higher fidelity methods at these conditions will reduce the cost and turn around time of the loads process of conventional aircraft. In addition, innovative designs required for greening aircraft can be evaluated more rapidly and at lower risk. Reduced order modelling techniques also offer the accuracy of high fidelity methods at a cost close to that of the current low fidelity methods. As a result, the proposed framework will be a high fidelity, multidisciplinary and real time analysis and optimization tool where the aerodynamics, structures, propulsion and control system dynamics are tightly coupled together to provide a virtual flight test capability. It can be employed to accurately predict aircraft loads and stresses for improved fatigue life and mitigate the cost of solving flight test related problems. The simulation framework will also be used for control law design, maneuvering flight simulation and handling quality assessment with the inclusion of nonlinear aeroelastic effects for high aspect ratio wings. The computational tools and processes developed will be validated and evaluated through a rigorous flight test program based on low cost flight test demonstrator models. The SAVANT design framework will be a valuable tool to design novel civil transportation aircraft and current and future Meggitt Training Systems Canada Unmanned Air Vehicles and will lead to a reduction of flight tests necessary for certification.
Program
Collaborative Research and Development Grants
Location
British Columbia, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data

As published

Application id
452988-2013
Name nom
Suleman, Afzal
Department département
Mechanical Engineering
Organization id
7
Institution établissement
University of Victoria
Province en
British Columbia
Province fr
Colombie-Britannique
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2014
Competition year année de concours
2013
Award amount
120000
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
Group en
Research partnerships programs
Group fr
Programmes de partenariat
Committee code
96
Committee name en
RPP Internal Decision Cttee
Committee name fr
Cté de décision interne - PPR
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
2100
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Mechanical engineering
Research subject fr
Génie mécanique
Partie
1
Nb partie
3
Application title
Multidisciplinary design optimization of novel aircaft configurations: stick-to-stress simulation, validation and evaluation (SAVANT)
Keyword
NSERC
Application summary
The proposed research program aims to develop a comprehensive virtual multidisciplinary stick-to-stress design optimization framework for the synthesis of novel and energy efficient aircraft configurations. SAVANT proposes to combine flight dynamic models and nonlinear aeroelastic solvers based on aerodynamic reduced order models (ROM) to generate ""in real-time"" loads and stresses resulting from pilot input commands. Critical load identification methods and reduced order modelling techniques will potentially provide a step change in the efficiency and accuracy of the dynamic aeroelastic loads process. Identifying the flight conditions that lead to the maximum loads on aircraft structures and introducing higher fidelity methods at these conditions will reduce the cost and turn around time of the loads process of conventional aircraft. In addition, innovative designs required for greening aircraft can be evaluated more rapidly and at lower risk. Reduced order modelling techniques also offer the accuracy of high fidelity methods at a cost close to that of the current low fidelity methods. As a result, the proposed framework will be a high fidelity, multidisciplinary and real time analysis and optimization tool where the aerodynamics, structures, propulsion and control system dynamics are tightly coupled together to provide a virtual flight test capability. It can be employed to accurately predict aircraft loads and stresses for improved fatigue life and mitigate the cost of solving flight test related problems. The simulation framework will also be used for control law design, maneuvering flight simulation and handling quality assessment with the inclusion of nonlinear aeroelastic effects for high aspect ratio wings. The computational tools and processes developed will be validated and evaluated through a rigorous flight test program based on low cost flight test demonstrator models. The SAVANT design framework will be a valuable tool to design novel civil transportation aircraft and current and future Meggitt Training Systems Canada Unmanned Air Vehicles and will lead to a reduction of flight tests necessary for certification.