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aeroelasticity PhD Projects, Programs & Scholarships

We have 6 aeroelasticity PhD Projects, Programs & Scholarships

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  Uncertainty Quantification in Aeroelasticity Using Reduced Order Models
University of Southampton Faculty of Engineering and Physical Sciences
  Research Group: Aerodynamics and Flight Mechanics
  Dr A Da Ronch
Application Deadline: 1 April 2019
Computational aeroelasticity to predict instabilities, such as flutter, incurs in high computing times and lacks reliability due to several sources of uncertainty.
Details
Type/Funding
  Development of CFD Methods for Future Digital Aircraft Design
University of Liverpool School of Engineering
  Dr S Timme
Application Deadline: 31 August 2019
Do you want to be part of the team that is developing the next-generation computational fluid dynamics (CFD) software solution to be used by Airbus and partner organisations across Europe in the next decades?.
Details
Type/Funding
  Hierarchical Optimization Approach to Detail Design of an Aircraft Wing
Cardiff University Cardiff School of Engineering
  Dr Alicia Kim
Application Deadline: 23 April 2019
This project will develop a hierarchical methodology to optimize an aircraft wing design. A unique novelty of the methodology that will be developed is that it will simultaneously optimize the overall wing mass and stiffness distribution as a subsystem and the detailed stiffener and skin components in a coupled way.
Details
Type/Funding
  Experimental Testing of Wing Loads Alleviation using Sloshing
University of Bristol Department of Aerospace Engineering
  Prof J Cooper
Application Deadline: 31 March 2019
The use of sloshing in aircraft wing fuel tanks to reduce the loading effects of gusts and turbulence has recently been identified.
Details
Type/Funding
  Investigation of Large Fold Angles of a Semi Aeroelastic Hinged Wing Tip
University of Bristol Department of Aerospace Engineering
  Prof J Cooper
Application Deadline: 31 March 2019
The Semi Aeroelastic Hinged wing tip concept has been developed by Airbus with the University of Bristol and is based on idea of allowing a wing-tip, that can be moved on the ground to fit airport gates, to be released for passive movement in-flight to enable gust loads alleviation & improved roll efficiency.
Details
Type/Funding
  Quasi-3D beam models for the nonlinear aeroelastic response of metallic and composite structures
University of Liverpool School of Engineering
  Dr F Fazzolari, Dr S Fichera
Application Deadline: 10 August 2019
This PhD project will focus on developing a quasi-3D beam models tailored to nonlinear aeroelastic systems that will be coupled to the aeroelastic suite of Nastran for extending its aeroelastic capabilities.
Details
Type/Funding
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