All Outputs (5)

The feasibility of hydrogen fuel cells as a solution toward zero emissions in general aviation aircraft (2023)
Presentation / Conference Contribution

In this chapter, hydrogen fuel cell (HFC) technology is investigated as a solution for the general aviation industry. A modified Cessna 172 installed with poly-membrane fuel cells (PEMFCs) was modelled through MATLAB/Simulink software with Hydrogen (... Read More about The feasibility of hydrogen fuel cells as a solution toward zero emissions in general aviation aircraft.

Evaluating the effects of a morphed trailing edge flap for aeroacoustics applications (2023)
Presentation / Conference Contribution

This chapter summarises the results of 2D CFD simulations of a 30P30N aerofoil section (without a leading edge slat) equipped with a morphing trailing edge flap (TEF). Numerical simulations are carried out at a fixed angle of attack of 8°, with f lap... Read More about Evaluating the effects of a morphed trailing edge flap for aeroacoustics applications.

Numerical framework for aerodynamic and aeroacoustics of bio-inspired UAV blades (2023)
Presentation / Conference Contribution

With the aim to understand and control the noise from small unmanned aerial vehicles (UAVs), this work presents a numerical framework for small-scale rotor blade, employing a bio-inspired finlet design. The simulation framework employs Direct Eddy Si... Read More about Numerical framework for aerodynamic and aeroacoustics of bio-inspired UAV blades.

A simplified digital twin framework of a trainer aircraft (2023)
Presentation / Conference Contribution

This paper aims to establish a simplified, user-friendly framework for a Digital Twin (DT) of a PC21 jet trainer aircraft. The implementation of the DT is carried out in Matlab with the aid of embedded Neural Network tools. The aircraft is trained a... Read More about A simplified digital twin framework of a trainer aircraft.

Aerodynamics of a CRM joined-wing configuration at transonic speeds (2023)
Presentation / Conference Contribution

The presented work aims to showcase a joined-wing (JW) concept with key design parameters based on the NASA Common Research Model (CRM) configuration, to highlight its potential application for an efficient commercial transport or cargo aircraft flyi... Read More about Aerodynamics of a CRM joined-wing configuration at transonic speeds.