“…The area, mass of the shaft, and volume of a flight are obtained with Eq. ( 25) to ( 27) respectively [34]. (25) (26) (27) where A s is the surface area of the shaft, r is the radius of the shaft, M s is the mass of the shaft, ρ is the density of the shaft, v is the volume of the shaft, V flight is the volume of a flight, L is the length of a flight (700 mm), b is the breadth of a flight (70 mm), and t is the thickness of a flight (3 mm).…”