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The use of natural fibers as reinforcement in polymeric composites is increasing thanks to the improvements in properties that fibers can provide to the merchandise. Composites materials were prepared by compression molding technique with hand layup process. Treatment of fiber with 2% NaOH was carried out in order to improve the interfacial bonds between fiber and matrix leading to better mechanical properties of the spathe-fiber-reinforced composite laminates. Filler loading as 5% by volume of coir fiber or epoxy resin composites have been formulated. The fiber length was chosen as 5mm, 10mm & 15mm and the ratio of epoxy resin: hardener was maintained as 10:0.8. A total three plates with dimension as 300 mm х 300 mm х 4 mm were produced and specimens as per the varied ASTM standard were tested to determine the ultimate tensile strength, strain energy, flexural strength, strain energy and micro hardness value for different configuration. It was observed that the lastingness of epoxy resin/ coir fiber composites was maximum at 15mm fiber length (16.27 N/mm2). The charpy notch impact strength was also maximum at 15mm fiber length (10.87 kJ/m2). The results show good mechanical properties and hint us as a replacement for conventional materials in industrial applications.

Processing processes such as petrochemical, refineries, pharmaceutical, thermal, chemical, and integrated chemical industries such as the food, dairy and sugar industries have been widely used for heat exchange. Additional techniques have been used in the formulation of various twist geometry gestures such as helical film, triangular/rectangular/trapezoidal tape, HiTrain wire matrix mould, a novel turbulator with a diameter (p/d), well placed/separated broken twisted tapes, conic splitting, and other geometric tapes are well researched with Reynolds number range 13–500,000 liquid processing solutions such as ethylene glycol and turbine oil respectively. This paper also highlighted the impact of circular holes, rectangular holes, angle of entry, wavy rate and tape size in the optimal temperature parameter such as thermal enhancement factor 1.04–3 varies with Reynolds' number from 100 to 20,000. By test/numerical reading the curved ratio was calculated from 0.25 short lengths to 20 trapezoidal cuts with tape geometry through various reviews. The Jacobean matrix associated to the linear equation is given by,$$\begin{aligned} J\left( X \right) & = \left[ { \begin{array}{*{20}c} {\frac{{\partial f_{1} }}{{\partial T_{2} }}} & {\frac{{\partial f_{1} }}{{\partial T_{4} }}} \\ {\frac{{\partial f_{2} }}{{\partial T_{2} }}} & {\frac{{\partial f_{2} }}{{\partial T_{4} }}} \\ \end{array} } \right] \\ \frac{{\partial f_{1} }}{{\partial T_{2} }} & = - Q_{h } Cp_{h} \\ \frac{{\partial f_{1} }}{{\partial T_{4} }} & = - Q_{c } Cp_{c} \\ \frac{{\partial f_{2} }}{{\partial T_{2} }} & = - Q_{h } Cp_{h} - \left\{ { \frac{{\left[ {U A \left\{ { \left( {T_{1} - T_{4} } \right) - \left( {T_{4} - T_{3} } \right) } \right\}} \right] \left[ { \frac{{\left( {T_{1} - T_{4} } \right)}}{{\left( {T_{2} - T_{3} } \right)}} } \right] ^{2 } }}{{\ln \left[ {\frac{{\left( {T_{1} - T_{4} } \right)}}{{\left( {T_{2} - T_{3} } \right)}}} \right] ^{2 } }}} \right\}. \\ \end{aligned}$$ J X = ∂ f 1 ∂ T 2 ∂ f 1 ∂ T 4 ∂ f 2 ∂ T 2 ∂ f 2 ∂ T 4 ∂ f 1 ∂ T 2 = - Q h C p h ∂ f 1 ∂ T 4 = - Q c C p c ∂ f 2 ∂ T 2 = - Q h C p h - U A T 1 - T 4 - T 4 - T 3 T 1 - T 4 T 2 - T 3 2 ln T 1 - T 4 T 2 - T 3 2 . Compared to a blank tube, the heat transfer rate and the friction factor improved by 20% when using full-length tapes y = 2.5, and NNu increased 9 times to y = 3.125. There is a 30–40% increase using different twisted tapes. This in-depth study is common use in industrial systems to gain power.