Dr Hamed Haddad Khodaparast

Research interests

Structural Dynamics
Uncertainty modelling, propagation and identification, probabilistic and non-probabilistic methods
Aeroelasticity: Flutter, gust response
Morphing aircraft
Active and Passive Vibration control
Robust design
Reduced Order Modelling
Composite structures

Publications

  1. Magrini, A., Benini, E., Ponza, R., Wang, C., Khodaparast, H., Friswell, M., Landersheim, V., Laveuve, D., Contell Asins, C., Haddad Khodaparast, H. Comparison of Constrained Parameterisation Strategies for Aerodynamic Optimisation of Morphing Leading Edge Airfoil Aerospace 6 3 31
  2. Jalali, H., Khodaparast, H., Madinei, H., Friswell, M., Friswell, M., Haddad Khodaparast, H., Madinei, H. Stochastic modelling and updating of a joint contact interface Mechanical Systems and Signal Processing 129 645 658
  3. Jalali, H., Khodaparast, H., Friswell, M., Haddad Khodaparast, H. The effect of preload and surface roughness quality on linear joint model parameters Journal of Sound and Vibration 447 186 204
  4. Nabavi, S., Farshidianfar, A., Afsharfard, A., Khodaparast, H., Haddad Khodaparast, H. An ocean wave-based piezoelectric energy harvesting system using breaking wave force International Journal of Mechanical Sciences 151 498 507
  5. Wang, C., Haddad Khodaparast, H., Friswell, M., Shaw, A., Xia, Y., Walters, P. Development of a morphing wingtip based on compliant structures Journal of Intelligent Material Systems and Structures 1045389X1878307

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Teaching

  • EG-260 Dynamics 1 (Mech & Aero)

    Elements of vibrating systems; simple harmonic motion; use of complex exponential representation. One-degree-of-freedom systems; natural frequency; effect of damping; harmonic excitation; rotating out-of-balance; vibration transmission. Transient dynamics; frequency domain analysis; impulse response function. Undamped multi-degree-of-freedom systems; Calculation of natural frequencies and mode shapes of two degree of freedom systems.

  • EG-M69 Advanced Airframe Structures

    Following a brief introduction to aircraft structures and structural components, the Advanced Aircraft Structures module covers advanced structural topics such as airframe loads and airworthiness, stress analysis of aircraft components (including wings and fuselages), structural idealisation, thin plate theory, applications of advanced composites in aircraft structures and aeroelasticity.

Supervision

  • Development of active and passive gust load reduction system considering non-linearity and uncertainty in the models (current)

    Student name:
    PhD
    Other supervisor: Dr Marinos Manolesos
    Other supervisor: Dr Hamed Haddad Khodaparast
  • Control Design of Flexible Link Robots with Smart Materials (current)

    Student name:
    PhD
    Other supervisor: Dr Shakir Jiffri
    Other supervisor: Dr Hamed Haddad Khodaparast
  • I've titled the journal paper that I am currently working on as "Wave Propagation in 1D and 2D Mechanical Metamaterials with Energy Harvesters". (current)

    Student name:
    PhD
    Other supervisor: Dr Hamed Haddad Khodaparast
    Other supervisor: Prof Sondipon Adhikari
  • Stochastic Nonlinear Model Updating in Structural Dynamics (current)

    Student name:
    PhD
    Other supervisor: Prof Michael Friswell
    Other supervisor: Dr Hamed Haddad Khodaparast
  • Stochastic Multiscale Methods for Failure Quantification in Advanced Composite Structures: Bottom-up approach«br /»«br /»«br /» (current)

    Student name:
    MSc
    Other supervisor: Dr Hamed Haddad Khodaparast
    Other supervisor: Prof Sondipon Adhikari
  • Modelling and Experimental Validation of Eddy Current Sensors for Blade Tip Timing (awarded 2019)

    Student name:
    PhD
    Other supervisor: Dr Hamed Haddad Khodaparast
    Other supervisor: Prof Michael Friswell
  • Design and optimisation of morphing aircraft (awarded 2018)

    Student name:
    PhD
    Other supervisor: Dr Hamed Haddad Khodaparast
    Other supervisor: Prof Michael Friswell
  • Analysis of nonlinear MEMS piezoelectric energy harvesters in the presence of manufacturing uncertainties (awarded 2018)

    Student name:
    PhD
    Other supervisor: Prof Sondipon Adhikari
    Other supervisor: Dr Hamed Haddad Khodaparast
  • 'Uncertainty quantification utilising MATLAB and FE modelling applied to composite structures' (awarded 2017)

    Student name:
    EngD
    Other supervisor: Prof Michael Friswell
    Other supervisor: Dr Hamed Haddad Khodaparast

Career History

Start Date End Date Position Held Location
2019 Present Associate Professor College of Engineering, Swansea University
2014 2018 Senior Lecturer College of Engineering, Swansea University
2013 2014 Lecturer College of Engineering, Swansea University
2012 2013 Research Officer College of Engineering, Swansea University
2011 2012 Research Associate School of Engineering, University of Liverpool
2007 2011 Research Assistant School of Engineering, University of Liverpool
2004 2007 Research Assistant Iran University of Science and Technology
1999 2004 Vibration Engineer AIRIC

Academic History

Date Qualification Location
2010 PhD University of Liverpool
2002 MSc Sharif University of Technology
1998 BSc Mechanical Engineering Ferdowsi University, Mashad

Key Grants and Projects

  • ‘Robust Gust Load Alleviation (RGLA) in composite aircraft structures’ Sêr Cymru National Research Network (NRN) Industrial Fellowship 2016 - 2017

    , £29,953

  • ‘Data-drive multidisciplinary design optimization of aircraft structures (MOAD) under uncertainty’ Sêr Cymru National Research Network (NRN) 2016 - 2017

  • British Council/Russia - Workshop in Uncertainty Quantification in Inverse Problems 2016

    , with £2000

  • Sêr Cymru National Research Network (NRN) industrial fellowship 2016

    , £900

  • ‘Efficient stochastic design (EStDe) of composite aircraft structures’, Royal Academy of Engineering Industrial Fellowship 2015 - 2016

    , £29,406

  • Funded by ESPRC - Stochastic nonlinear aeroelastic models subject to unsteady loads 2017 - 2019

    , £124,697

  • Funded by ATI/ESPRC - Exploiting Aeroelastic Deflections For Improved Aircraft Performance 2016

    , £19,600

  • Funded by ERC/Clean Sky - Development of Methods for Deriving Optimized Shapes of Morphing Structures Considering both Aerodynamic Performance and Specific Mechanical Morphing Boundary Conditions (OPTIMOrph) 2017 - 2019

    , £113,875

  • Funded by NRN - Travel Grant 2017 - 2018

    , £10,000