Dr Gareth Vio

Lecturer

J11 - Aeronautical Engineering Building
The University of Sydney

Telephone +61 2 9351 2394
Fax +61 2 9351 4841

Teaching and supervision

AERO1560 - Introduction to Aerospace Engineering

AERO3260 - Aerodynamics 1

AERO5210 - Foundations of Aerodynamics

AMME5510 - Vibration and Acoustics

Selected grants

2014

  • Modelling of Fluid-Structure Interaction; Vio G; Defence Science and Technology Organisation/Contract Research Agreement.

Selected publications

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Journals

  • Georgiou, G., Vio, G., Cooper, J. (2014). Aeroelastic tailoring and scaling using bacterial foraging optimisation. Structural and Multidisciplinary Optimization, Published online: 8 February 2014(50), 81-99. [More Information]
  • Morrell, B., Munk, D., Vio, G., Verstraete, D. (2014). Development of a Hypersonic Aircraft Design Optimization Tool. Applied Mechanics and Materials, 553(2014), 847-852.
  • Vio, G., Verstraete, D. (2014). Development of a Hypersonic Aircraft Design Optimization Tool. Applied Mechanics and Materials, accepted ACCM2013 paper-published in spl ed.
  • El Tom, J., Vio, G. (2014). Novel Wing Box Design. Applied Mechanics and Materials, 553(2014), 243-248. [More Information]
  • Giannelis, N., Vio, G., Verstraete, D. (2014). Temperature Effect on the Structural Design of a Mach 8 Vehicle. Applied Mechanics and Materials, 553(2014), 249-254. [More Information]
  • Amoozgar, M., Irani, S., Vio, G. (2013). Aeroelastic instability of a composite wing with a powered-engine. Journal of Fluids and Structures, 36, 70-82. [More Information]
  • Khodaparast, H., Georgiou, G., Cooper, J., Riccobene, L., Ricci, S., Vio, G., Denner, P. (2012). Efficient Worst Case "1-Cosine" Gust Loads Prediction. Journal of Aeroelasticity and Structural Dynamics (ASDJournal), 2(3), 33-54. [More Information]
  • Manan, A., Vio, G., Harmin, M., Cooper, J. (2010). Optimization of aeroelastic composite structures using evolutionary algorithms. Engineering Optimization, 42(2), 171-184. [More Information]
  • Gu, Z., Oyadiji, S., Vio, G. (2009). Fuzzy Adaptive control of Hysteretic Based-Isolated Structural System Under Seismic Disturbances. International Journal of Applied Mathematics and Mechanics, 5(1), 89-101.
  • Vio, G., Dimitriadis, G., Cooper, J., Badcock, K., Woodgate, M., Rampurawala, A. (2007). Aeroelastic system identification using transonic CFD data for a wing/store configuration. Aerospace Science and Technology, 11(2-3), 146-154. [More Information]
  • Vio, G., Dimitriadis, G., Cooper, J. (2007). Bifurcation analysis and limit cycle oscillation amplitude prediction methods applied to the aeroelastic galloping problem. Journal of Fluids and Structures, 23(7), 983-1011. [More Information]
  • Dimitriadis, G., Vio, G. (2007). Demonstrating the identification of nonlinear vibrating systems to undergraduate students. International Journal of Mechanical Engineering Education, 35(4), 336-360.
  • Henshaw, M., Badcock, K., Vio, G., Allen, C., Chamberlain, J., Kaynes, I., Dimitriadis, G., Cooper, J., Woodgate, M., Rampurawala, A., et al (2007). Non-linear aeroelastic prediction for aircraft applications. Progress in Aerospace Sciences, 43(4-6), 65-137. [More Information]
  • Gu, Z., Vio, G., Oyadiji, S. (2007). Vibration Control of Nonlinear System Using RBF-Based Sliding Mode Control. International Journal of Applied Mathematics and Mechanics, 3(4), 56-68.
  • Vio, G., Cooper, J. (2005). Limit Cycle Oscillation Prediction for Aeroelastic Systems with Discrete Bilinear Stiffness. International Journal of Applied Mathematics and Mechanics, 3, 100-119.

Conferences

  • Kukreja, S., Vio, G., Andrianne, T., Razak, N., Dimitriadis, G. (2012). A Cross-Validation Approach to Approximate Basis Function Selection of the Stall Flutter Response of a Rectangular Wing in a Wind Tunnel. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Worotynska, J., Vio, G. (2012). Aeroelastic Response of Chordwise Flexible Wings Subjected to Gusts: An Initial Study On Experimental and Computational Validation. 28th Congress of the International Council of the Aeronautical Sciences (ICAS 2012), UK: Optimage Ltd.
  • Vio, G. (2012). Bifurcation Prediction of the Aeroelastic Galloping Model with Structural and Damping Non-Linearities. 15th Australasian Wind Engineering Society (AWES) Workshop, Sydney, Australia: AWES (Australasian Wind Engineering Society).
  • Vio, G., Dimitriadis, G. (2012). Computational Identification of Non-Linear Damping in an Aeroelastic System. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Vio, G., Fitzpatrick, I. (2012). Design of Composite Structures for Improved Aeroelastic Performance. 28th Congress of the International Council of the Aeronautical Sciences (ICAS 2012), UK: Optimage Ltd.
  • Vio, G., Georgiou, G., Cooper, J. (2012). Design of Composite Structures to Improve the Aeroelastic Performance. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Vio, G., Worotynska, J., Berci, M., Dimitriadis, G. (2012). Initial Investigation of Chordwise Flexible Flat Aerofoil. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Vio, G., Stanley, D. (2012). Non-Linear Behaviour of a Wing Due to Underwing Stores. 28th Congress of the International Council of the Aeronautical Sciences (ICAS 2012), UK: Optimage Ltd.
  • Verstraete, D., Vio, G. (2012). Temperature effects on flutter of a Mach 5 transport aircraft wing. ASME 2012 International Mechanical Engineering Congress and Exposition, Houston, Texas: American Society of Mechanical Engineers (ASME).
  • Vio, G., Dimitriadis, G. (2011). Damping Identification in an Aeroelastic System with Structural Non-Linearities. AIAC-14 Fourteenth Australian International Aerospace Congress APISAT 2011, Melbourne, Australia: WALDRONSMITHManagement.
  • Vio, G., Miller, S., Cooper, J. (2011). Gust Alleviation Device Applied to the Sensorcraft Structure. AIAC-14 Fourteenth Australian International Aerospace Congress APISAT 2011, Melbourne, Australia: WALDRONSMITHManagement.
  • Khodaparast, H., Georgiou, G., Cooper, J., Travaglini, L., Ricci, S., Vio, G., Denner, P. (2011). Rapid Prediction of Worst Case Gust Loads. 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, USA: American Institute of Aeronautics and Astronautics (AIAA).

2014

  • Georgiou, G., Vio, G., Cooper, J. (2014). Aeroelastic tailoring and scaling using bacterial foraging optimisation. Structural and Multidisciplinary Optimization, Published online: 8 February 2014(50), 81-99. [More Information]
  • Morrell, B., Munk, D., Vio, G., Verstraete, D. (2014). Development of a Hypersonic Aircraft Design Optimization Tool. Applied Mechanics and Materials, 553(2014), 847-852.
  • Vio, G., Verstraete, D. (2014). Development of a Hypersonic Aircraft Design Optimization Tool. Applied Mechanics and Materials, accepted ACCM2013 paper-published in spl ed.
  • El Tom, J., Vio, G. (2014). Novel Wing Box Design. Applied Mechanics and Materials, 553(2014), 243-248. [More Information]
  • Giannelis, N., Vio, G., Verstraete, D. (2014). Temperature Effect on the Structural Design of a Mach 8 Vehicle. Applied Mechanics and Materials, 553(2014), 249-254. [More Information]

2013

  • Amoozgar, M., Irani, S., Vio, G. (2013). Aeroelastic instability of a composite wing with a powered-engine. Journal of Fluids and Structures, 36, 70-82. [More Information]

2012

  • Kukreja, S., Vio, G., Andrianne, T., Razak, N., Dimitriadis, G. (2012). A Cross-Validation Approach to Approximate Basis Function Selection of the Stall Flutter Response of a Rectangular Wing in a Wind Tunnel. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Worotynska, J., Vio, G. (2012). Aeroelastic Response of Chordwise Flexible Wings Subjected to Gusts: An Initial Study On Experimental and Computational Validation. 28th Congress of the International Council of the Aeronautical Sciences (ICAS 2012), UK: Optimage Ltd.
  • Vio, G. (2012). Bifurcation Prediction of the Aeroelastic Galloping Model with Structural and Damping Non-Linearities. 15th Australasian Wind Engineering Society (AWES) Workshop, Sydney, Australia: AWES (Australasian Wind Engineering Society).
  • Vio, G., Dimitriadis, G. (2012). Computational Identification of Non-Linear Damping in an Aeroelastic System. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Vio, G., Fitzpatrick, I. (2012). Design of Composite Structures for Improved Aeroelastic Performance. 28th Congress of the International Council of the Aeronautical Sciences (ICAS 2012), UK: Optimage Ltd.
  • Vio, G., Georgiou, G., Cooper, J. (2012). Design of Composite Structures to Improve the Aeroelastic Performance. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Khodaparast, H., Georgiou, G., Cooper, J., Riccobene, L., Ricci, S., Vio, G., Denner, P. (2012). Efficient Worst Case "1-Cosine" Gust Loads Prediction. Journal of Aeroelasticity and Structural Dynamics (ASDJournal), 2(3), 33-54. [More Information]
  • Vio, G., Worotynska, J., Berci, M., Dimitriadis, G. (2012). Initial Investigation of Chordwise Flexible Flat Aerofoil. AIAA 53rd Structures, Structural Dynamics, and Materials Conference, Hawaii: American Institute of Aeronautics and Astronautics (AIAA).
  • Vio, G., Stanley, D. (2012). Non-Linear Behaviour of a Wing Due to Underwing Stores. 28th Congress of the International Council of the Aeronautical Sciences (ICAS 2012), UK: Optimage Ltd.
  • Verstraete, D., Vio, G. (2012). Temperature effects on flutter of a Mach 5 transport aircraft wing. ASME 2012 International Mechanical Engineering Congress and Exposition, Houston, Texas: American Society of Mechanical Engineers (ASME).

2011

  • Vio, G., Dimitriadis, G. (2011). Damping Identification in an Aeroelastic System with Structural Non-Linearities. AIAC-14 Fourteenth Australian International Aerospace Congress APISAT 2011, Melbourne, Australia: WALDRONSMITHManagement.
  • Vio, G., Miller, S., Cooper, J. (2011). Gust Alleviation Device Applied to the Sensorcraft Structure. AIAC-14 Fourteenth Australian International Aerospace Congress APISAT 2011, Melbourne, Australia: WALDRONSMITHManagement.
  • Khodaparast, H., Georgiou, G., Cooper, J., Travaglini, L., Ricci, S., Vio, G., Denner, P. (2011). Rapid Prediction of Worst Case Gust Loads. 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, USA: American Institute of Aeronautics and Astronautics (AIAA).

2010

  • Manan, A., Vio, G., Harmin, M., Cooper, J. (2010). Optimization of aeroelastic composite structures using evolutionary algorithms. Engineering Optimization, 42(2), 171-184. [More Information]

2009

  • Gu, Z., Oyadiji, S., Vio, G. (2009). Fuzzy Adaptive control of Hysteretic Based-Isolated Structural System Under Seismic Disturbances. International Journal of Applied Mathematics and Mechanics, 5(1), 89-101.

2007

  • Vio, G., Dimitriadis, G., Cooper, J., Badcock, K., Woodgate, M., Rampurawala, A. (2007). Aeroelastic system identification using transonic CFD data for a wing/store configuration. Aerospace Science and Technology, 11(2-3), 146-154. [More Information]
  • Vio, G., Dimitriadis, G., Cooper, J. (2007). Bifurcation analysis and limit cycle oscillation amplitude prediction methods applied to the aeroelastic galloping problem. Journal of Fluids and Structures, 23(7), 983-1011. [More Information]
  • Dimitriadis, G., Vio, G. (2007). Demonstrating the identification of nonlinear vibrating systems to undergraduate students. International Journal of Mechanical Engineering Education, 35(4), 336-360.
  • Henshaw, M., Badcock, K., Vio, G., Allen, C., Chamberlain, J., Kaynes, I., Dimitriadis, G., Cooper, J., Woodgate, M., Rampurawala, A., et al (2007). Non-linear aeroelastic prediction for aircraft applications. Progress in Aerospace Sciences, 43(4-6), 65-137. [More Information]
  • Gu, Z., Vio, G., Oyadiji, S. (2007). Vibration Control of Nonlinear System Using RBF-Based Sliding Mode Control. International Journal of Applied Mathematics and Mechanics, 3(4), 56-68.

2005

  • Vio, G., Cooper, J. (2005). Limit Cycle Oscillation Prediction for Aeroelastic Systems with Discrete Bilinear Stiffness. International Journal of Applied Mathematics and Mechanics, 3, 100-119.

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