Areas of research for Deakin MAHE Cotutelle PhD Program Natural Fibre Based Hybrid Composite Material for all weather UAV application In the present era, significant and rapid developments are taking place in the field of composites resulting in the discovery of improved material system designed to meet the requirements. Traditional composite structures, which are reinforced by synthetic fibres namely, glass, aramid and carbon fibres are expensive and also harmful to the environment. Due to these reasons, natural fibres are gaining traction, which put forwards certain properties like low weight, abundant availability, renewable in nature, increased biodegradability, good strength, reduced cost and environment friendly. Natural fibres thus are becoming an alternative reinforcement over synthetic fibres in making of composite material, which can be used for several applications, which include automobile parts, household appliances, furnitures, in packaging, light to moderate loaded structural applications, Unmanned Aerial Vehicles, personal protective armours, etc. [1]. Natural fibres are obtained from the nature and can be classified into two categories, plant based and animal based. Some of the properties that make natural fibres an attractive alternative to synthetic fibres are low cost, light weight, minimal health hazards during processing, biodegradable, reasonably good specific strength and modulus, good thermal and acoustic insulation characteristics, ease of availability, etc. One of the major limitations of natural fibre as reinforcing material is that it is hydrophilic in nature, which makes them incompatible with polymers. The result of this incompatibility can be seen in weak bonding with the matrix resulting in inconsistent and reduced mechanical properties. To overcome this, fibres have to be modified with surface treatment that results in enhanced adhesion with the matrix. During chemical treatment formation of new moieties and activation of hydroxyl groups takes place, which brings about an effective interlock mechanism with the matrix [2]. In addition to chemically treating the fibres, they may be treated with certain coupling agents in order to enhance its bonding with the matrix [3, 4]. (Sarfi et al. 2017; Mohammed et al. 2015). UAVs are supposed to be light in weight and thus Aluminium presently is the first choice material for building the same. Some of the other properties that are required in UAVs other than lower weight are good mechanical properties, resistance to impact, fatigue and corrosion, minimal machining, easy fabrication of intricate parts, low absorption of radar and microwave to provide stealth capabilities, low coefficient of thermal expansion, etc. Other than these properties, UAVs should be inexpensive. Use of lightweight advances composites has thus become essential. Lightweight material will also enhance flight time. Some of the reinforcements that are being used presently are S-glass, E-glass, Aramid, Carbon, High Molecular Weight Polyethelene while among the matrix, epoxy, vinyl ester, polyester, phenolic and polyimide resins are being used. Composites have the potential to reduce the overall UAV weight by 15-45% depending on the extent of composite use. In order to reduce the weight to above 50% improvements in composite economics is required. Use of suitable natural fibres along with synthetic fibres and micro/ nano fillers can help in overcoming the above mentioned challenges in the area of use of composite material for all weather UAVs. Eligibility and Desirable qualifications 1. Above 70% Master’s degree in Mechanical/Manufacturing engineering. 2. Good communication and writing skills as evidenced from research publications or Master’s thesis 3. Possess strong data analysis skills and good knowledge of statistics