70kW Automobile Radiator for Light Duty Passenger Vehicle By S.W.A.S.T. SAMARATHUNGA Department of Mechanical Engineering University of Moratuwa Sri Lanka 18th May 2022 ABSTRACT Internal combustion engine serves as the prime mover of automobile even after the centuries of it’s first use in the cause. However, regulating the temperature of the engine by effectively removing the excess heat generated in the combustion process is vital for the safe and sustainable operation of the system. Therefore, Radiator, a special heat exchanger which has been developed overtime for the above requirement is delivering a critical service to the function of an automobile. In this report, designing a radiator with a capacity of 70kW, for a light duty passenger vehicle is analysed. INTRODUCTION Automobile, first being invented as a motored substitute to the horse carriages for a transport medium, subjected into a tremendous evolution over the past century. In it’s journey of pushing the performance boundaries further and further, the cooling of internal combustion engine which powered the automotive also played a major role. Engine cooling is not a factor to be overlooked as it mainly affects the engine as the too high temperatures causes metal weakening in overheated engine parts, viscosity breakdown of the lubricating oils and accelerated wear of engine parts due to the build up stress between those parts ultimately resulting in knocking, cylinder deformation and piston deformation. Thus, the air-cooled heat exchangers specifically ‘Radiators’ are being employed in every automobile cooling system. Automobile cooling system basically consist of radiator, water or coolant pump, electric cooling fan, pipe system, radiator pressure cap, and thermostat. Further, heater core is also included in the system to direct the engine heat into the passenger cabin for cabin heating purpose. To identify radiator’s function of rejecting out the accumulated heat from coolant to the outer environment, let’s investigate the overall function of automotive cooling system. The coolant is being circulated through the coolant channels made in engine body around the combustion cylinders where the major heat generation occurs. When the temperature of the coolant rises to a certain level, thermostat opens the path for coolant to flow through radiator, with the help of circulating pump, operates with the help of crank shaft motion. Control of this thermostat is being undertaken by the car’s ECU in modern vehicles. When the coolant flows through the radiator pipes, the heat is effectively dissipated to the air flowing through the radiator fins due to either the motion of the automobile, or the radiator fan, which is an inward draft axial fan, located right behind the radiator. The pressure regulating valve on the top of the radiator is to let the excess coolant flow into the reservoir bottle in a case of increased pressure of coolant inside the radiator. The cooled coolant is then flowing back into the engine block to complete the cycle. While this process continues, if the passenger compartment requires to be heated, required amount of coolant is to be flown through a secondary heat exchanger, where the draft flowing through the exchanger routed into the passenger compartment. Further, some oil cooling arrangements are also available in the overall cooling process but those can be overlooked for the Figure1:Automobile Cooling system with the Primary and secondary working fluid flows sake of simplicity of the context. Radiators were hand-built individually until around 1910, when the factory-built radiators were started to appear in automobile. In around 1940, the passenger compartment heaters were integrated into the vehicles and in 50th decade, automobiles equipped with Air conditioning systems started to appear in the automobile market. Further, advancements made in internal combustion engine technologies in latter decades such as super chargers and turbo chargers highlighted the need of effective cooling of the engine walls thus, the evolution of radiators occurred as a result. A peek at this evolution journey is beneficial in understanding the major changes to the radiator throughout the history. Radiator Material From early days, radiators made of Copper or Brass (made of brass and lined with copper) was used in automobile. Given the high thermal capacity of copper and Brass, an alloy of copper, these devices were reliable but at the same time, were bulky and weighed a lot. Therefore, despite the reliability, with the advancements of automobile technology and prioritizing of lighter weight, radiator manufacturing material moved away from copper and it’s alloys to Aluminium, a rather lighter and better option. Today, aluminium radiators are dominating the high-performance car radiator market where both core of the radiator and the coolant tanks are made of lighter aluminium. Further, there are plastic radiators in the market where the tanks are made of plastic while the core of the radiator still being made of an alloy or metal. However, these plastic radiators are not as efficient as the aluminium ones and further, the build of such plastic arrangement as a radiator demands the need of entire replacement if a problem arises in the device. In Al made radiators, this can be easily tackled by replacing the problematic part only, eliminating the need of entire radiator replacement. However, what is being utilized most in modern, general use cars is a hybrid plastic_ aluminium structure, which produce the advantages of both designs while trying to eliminate the adverse effects of each. Tube Arrangement Radiator being a passive device, rejects out whatever heat that comes to it through coolant. The coolant temperature which is exiting through the outlet of the radiator depends on the radiator’s capacity of heat rejection. If the capacity is less, the outlet coolant line may be still in a higher temperature than needed, causing inefficient cooling in engine walls. If the capacity is redundant, the coolant will be cooled to a temperature lower than acceptable or unnecessary. In earlier times, most of the radiators were made from copper fins and brass tubes where flat tubes and corrugates louver fin design was used. Later during World War II, Russian tankers were using circular tubes with flat fin aluminium radiators, and this design was later popularized in Europe for smaller engines. But, even today, Flat pipe design with Corrugated fins is being utilized using Aluminium as the manufacturing material. Further, the early day’s radiators were downflow radiators where the coolant tubes were vertical where coolant flows from top to bottom. But later, the cross-flow radiators gained the popularity with its added advantages of having same tank and header design despite the length of the coolant tube channels, thus enabling the ability to adapt the design for more frontal area with lesser effort and etc. However, since 90’s the downflow radiators are again gaining the popularity due to characteristics like lower coolant pressure drop and pumping power, and flexibility in attachments. In addition to above information, the coolant used in radiators is also have evolved, where a 5050 mix of water and ethylene glycol is used along with some additives to give the liquid aspired properties of lower freezing point, higher thermal capacity and while avoiding adverse properties like casing rust. To ensure proper heat transfer from the coolant to the air, the coolant flow inside the radiator tubing has to be turbulent where the mixing of the coolant is ensured. To achieve this, structures names vortex generators are inserted in the radiator tubing. Usually for round tubes rathe simple structures like coiled wires or balls are being used while for flat tubes, special structures are available. METHODOLOGY Materials and dimensions of the radiator design were chosen according to the current standards and conventions. Since the aspired design is a coolant cross flow one, the length of the radiator tubes was considered the main variable, while number of tube rows and columns were finalized after iterations of calculations for the appropriate length of the radiator After the selection of flow rates of coolant pump and flow fans, which were again done iteratively while taking the help of available literature, thermal properties of both coolant and air sides were obtained using property tables. Since the required capacity of the radiator is 70kW, required UA value was calculated using the NTU method. Mass flow rates are calculated from volume flow rates: πΜπππ , πΜπππππππ‘ With the specific heat capacities ππππ and ππππππππ‘ , πΆπππ = πΜπππ x ππππ and πΆπππππππ‘ = πΜπππππππ‘ x ππππππππ‘ were calculated. Using those, πΆπ = πΆπππ ππππ₯ = πΆπππ (πβππ‘,ππ − πππππ,ππ ) thus, effectiveness(ε) = , πΆπππ₯ πππππ’ππππ ππππ₯ Using the standard equation for effectiveness for an cross flow heat exchanger in NTU method, NTU value can be found. ε = {1 − π ( 0.78 ) 1 πππ 0.22 )(π (−πΆπ πππ −1) πΆπ } But, NTU = ππ΄ πΆπππ , Therefore, required UA for the radiator is found. Heat transfer Ratios for both liquid(Coolant) side and the air side is then calculated. Liquid Side: From the flow rate, flow velocity Vcoolant was found and Re number for the velocity is found. Nusselt number is then found accordingly to a internal flow of square shaped tube and hence the hcoolant was found. Air Side: Air side heat transfer coefficient was also found similarly, but the length of the radiator remains as a variable in the equations here, as it is associates with the flow area concerned to find the Vair. Here also, the flow nature was considered by the value of Reynold’s number and the Nusselt number equation was chosen accordingly. Since the utilization of fins in a radiator is quite significant the overall surface efficiency must be calculated for the external area. For that, fin efficiency was calculated priorly. Fin efficiency (ππππ ) = m = √πΎ βπππ ππππ tanh(ππΏ) ππΏ and π΄π π΄πππ,ππππ L = height of the fin (Pfin: perimeter of the fin) Here, a fair assumption was made that the fins have adiabatic fin tips as given the fin positioning in a radiator, where the two consecutive tubes share the same fin tip, literally composing a insulated fin tip condition. Further, even though the fins possess a sinusoidal shape in realty, a straight rectangular shape has assumed for the sake of simplicity in calculating. Overall surface efficiency: π π0 = 1 − π΄ πππ π΄πππ πππ+πππ π (1 − ππππ ) Nfin = Number of Fins Afin = Surface area of the fin face Afin+base = (Nfin x Afin) + Abase Abase = Aradiator – Afin face Hence, −1 1 1 )+ ( )] ππ΄ = [( π0 βπππ π΄ππ₯π‘πππππ βπππππππ‘ π΄πππ‘πππππ Aexternal = Afin+base Ainternal = Inner area of the tubes Since the required UA value is known from the NTU method, the only variable remaining, the length of the radiator tubes can be obtained. However, to get a practically viable length, few iterations while changing the other parameters had to be done. CALCULATION Given the capacity of the radiator(70kW), an all-Aluminium design was chosen adopting the modern performance car radiators where the fins, tubing and the casing would be made of Aluminium with cross coolant flow design. 1.8mm 19.6mm Radiator tube specifications: Thickness - 0.18mm 10mm 6mm Radiator Fin Specifications: Thickness - 0.1mm All the specifications were considered adhering to the currently used industrial standards and conventions, to ensure the validity of the designs. Number of Tube lines = 240; Rows – 80, Columns - 3 Thus, Radiator Height - 630mm Radiator Thickness - 68.8mm Generally available specifications: Tube Area (As) : 35.3 x 10-6 m2 Tube Hydraulic Diameter (Dh) : 4As/P = 3.3 x 10-3 mm Inlet Hose Diameter : 31.75mm (1.25”) Fan Diameter : 0.3048m Number of Fans Used : 2 Coolant liquid Side: Coolant flowing the in the radiator tube is considered as the 50% ethylene glycol which is the generally used radiator coolant. Flow rate of the pump : 60 Litres per Minute (1x10-3 m3s-1) [Obtained from similar literature] Inlet Temp. : 950C Outlet Temp. : 250C βΈ« Average Temperature : 600C For the obtained Tavg thermal properties of 50% ethylene glycol was obtained referring available thermal property tables For T = 600C, Density(ρ) : 1031.114kgm-3 Dynamic Viscosity : 0.001198 kg/m.s Specific Heat Capacity : 3.386 kJ/kg.K Thermal Conductivity : 0.458 W/m.K Prandtl Number : 8.8596 Air Side: Flow rate of the selected fans : 4000 (2000x2) CFM (1.89 m3/s) [Obtained from data sheets] : 350C Density(ρ) : 1.146kgm-3 Dynamic Viscosity : 1.891 x 10--5 kg/m.s Specific Heat Capacity : 1.0067 kJ/kg.K Thermal Conductivity : 0.0267 W/m.K Prandtl Number : 0.7129 Ambient Air Temperature For T = 350C, Air Temperature for the properties were taken at a slightly higher value than the ambient temperature to compensate the errors. πΜπππ = 1.146πππΜ −3 × 1.89π3 π −1 = 2.17πππ −1 πΆπππ = πΜπππ × ππππ = 2.17πππ −1 × 1.0067ππ½/πππΎ = 2.185ππ½/π πΎ Μ −3 × (1π − 3)π3 π −1 = 1.03πππ −1 πΜπππππππ‘ = 1031.114πππ πΆπππππππ‘ = πΜπππππππ‘ × ππππππππ‘ = 1.03πππ −1 × 3.386ππ½/πππΎ = 3.49ππ½/π πΎ ∴ πΆπππ = 2.19ππ½/π πΎ πΆπ = 0.63 ππππ₯ = 2.19(95 − 25) = 153.3ππ π= ε = {1 − π ( 70 = 0.46 153.3 0.78 ) 1 πππ 0.22 )(π (−πΆππππ −1) πΆπ 1 0.46 = {1 − π (0.63πππ } 0.22 )(π (−0.63πππ0.78 ) −1) } ππ΄ NTU = 0.79 = 2.19 ∴ ππ΄π πππ’ππππ = 1.73ππ Heat Transfer Coefficients Since Volume flow rate of coolant, πΜ = 1 x 10-3 m3/s, taking the effective cross-sectional area of the all the pipes, the coolant flow velocity inside the radiator pipes is found. ππππππππ‘ 1 × 10−3 = = 0.12ππ −1 35.3 × 10−6 × 240 π π = πππ· π = 1021.114 ×0.12×3.3×10−3 0.001198 = 340.27 340.27 < 3000 Even though the Re number falls in the laminar range, with the presence of turbulators inside the tubes, the turbulence is induced in real situation. But since turbulators has been omitted in the design, flow is considered to be laminar. Nussult number for a internal laminar flow through a rectangular tube with similar aspect ratio lies at a constant value of 5.6 hcoolant = π ππ’ π· = 0.458 × 5.6 3.3 × 10−3 ππππ = = 777.2 W/m2K ππππ π΄ππππππ‘ππ − π΄π‘π’πππ 1.89π3 π −1 = (0.63 × πΏ) − (((1.8 + 2 × 0.18) × 10−3 ) × πΏ × 80) = 4.1 πΏ Reynolds number is calculated assuming the flat tubes as flat plates π π = πππ· π = 4.1 ×19.6×10−3 πΏ 1.891×10−5 1.146 × = 4870 πΏ Assuming L < 1m, flow is considered to be laminar Nusselt Number (Nu) = β π·π’ π = 0.664 x Re0.5 x Pr0.33 = 0.664 x (4870/πΏ)0.8 0.7130.33 = 41.4/√πΏ Therefore, convective heat transfer coefficient, hair = π ππ’ π· = 0.0267 × 41.4/√πΏ 19.6 × 10−3 = 55.8/√πΏ W/m2K To get the U for the finned surface, let’s consider the geometry of the radiator. 630mm For the simplicity in calculation, fins are to be considered as flat straight plates with width of 19.6mm same as the tube widths and thickness of 0.01mm, rather than sinusoidal ones. π= βπππ × π 2βπππ ≈ πΎπ΄π × π΄πππ πΎπ΄π × π»πππ π= 70.35 4 √πΏ KAl = 237W/m.k 4 Assuming √πΏ = 1, π = 70.35 ππππ = tanh(0.422) = 0.945 0.422 Number of fins per unit length = 800 fins/m Therefore, total number fins = 800 x L x (80 x 3) = 192,000 x L Afin = 2 x 19.6mm x 6mm = 2.352x 10-4m2 AB = 2 Lradiator Wtube N – HfinWfinNfin = Afin+base = NfinAfin + AB = (49.45 x L) m2 NfinAfin = (45.12 x L) m2 π0 = 1 − [ 45.12 (1 − 0,945)] 49.45 π0 = 0.95 For to obtain the UA value, −1 1 1 ππ΄ = [ + ] π0 βπππ π΄ππ₯π‘πππππ βπππππππ‘ π΄πππ‘πππππ Aexternal = Afin base x Ntube = (49.45 x L) m2 Ainternal = (2Wtube +2Htube)LradiatorNtube = (10.27 x L) m2 1 −1 1 1730 = [ + ] 777.2 × 10.27πΏ 0.954 × 55.8/√πΏ × 49.45πΏ Lradiator = 0.95m 3D MODEL AND COMPUTATIONAL FLUID DYNAMICS ANALYSIS A 3d model with obtained dimensions was developed using SOLIDWORKSTM and simulated in using Ansys FluentTM. However, due to extreme complexity in the geometry from the possession of very thin fins, the computational power required for the entire model was not available. Further, the need of simulating the entire model seemed bit redundant in the context of the requirement. Thus, a slice of the radiator, comprising one tube with its fins on each side was modelled and used in simulating software. The major drawback of this simplification is the missing out of effect of parallelly placed tubes affecting each other’s air flow and air temperature. However, provided the large air volume swept through the radiator fins as well as the relatively smaller radiator thickness, the mentioned effect can assume to be negligible. A major step to reduce the effect was designing the fluid domain, slightly omitting the tips of the fins, such a way that it the prevents the convective heat absorption from the air domain to the fins through the irrelevant fin tips. 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