Matthew Schrandt MES 601 Final Test Physical Chemistry Test 1. The contact angle between hexadecane and n-hexatriacontane (C36H78, solid) is 46 degrees. LV for hexadecane is 27.6 mJ/m2. What is the work of adhesion between hexadecane and n-hexatriacontane? (hexadecane-hexatriacontane) = 46° (hexadecane-air) = 27.6 mJ/m2 ( ( ) )( ( )) Assuming the sl between hexadecane and n-hexatriacontane is equivalent to that of decane (lv = 23.9 mJ/m2) and n-hexatriacontane, what is the decane - n-hexatriacontane contact angle? ( ( ) ) ( ( ) ) ( ) Do you think this is a reasonable assumption? Why? Would it be a reasonable assumption if water were the liquid rather than decane? Yes, this is a reasonable assumption, the surface tensions (γ) between the liquids is close and the angles used are fairly close. This means that decane and hexadecane are fairly close. However, water would be a bad substitute since the surface tension which is a lot higher. This makes sense as well since water has a completely different chemical structure and properties whereas hexadecane and decane have similar properties due to their chemically similar structures. 2. From the data below, compare the solid surface energy components for automobile parts painted with an acrylic paint and a urethane-based paint using two different furnace types. Which paint and furnace will give the best adhesion between the paint and metal surface. Contact Angle gas urethane acrylic electric urethane acrylic Work gas Bake time 0.75 2 4 0.75 2 4 0.75 2 4 0.75 2 4 CH2I2 48.3 50.5 53.8 49.3 50.3 53.5 39.7 40.1 41.1 19.7 30.8 44.3 H2O 88.1 97.4 98.1 92.7 94.5 96.9 81.6 83.5 90.3 82 84.1 87 C2H6O2 74.2 75.5 78.6 73.6 75.9 78.9 69.2 70.5 72.6 69.9 70.5 71.4 γ 50.8 72.8 48 urethane acrylic electric urethane acrylic CH2I2 84.5937 83.11277 80.80277 83.9266 83.24941 81.017 89.8855 89.65801 89.08102 98.6267 94.43516 87.15719 H2O 75.2137 63.42368 62.54239 69.37065 67.08818 64.05404 83.43484 81.04119 72.41882 82.9318 80.2833 76.61006 C2H6O2 61.06945 60.01824 57.48755 61.55239 59.69352 57.24105 65.04513 64.02273 62.35396 64.49567 64.02273 63.31005 Maximum work is best paint. The maximum work occurs for the acrylic paint in the electric oven for CH2I2 (w=98.6267 mJ/m2). From the trends observed in the chart above, the values for the electric ovens vs those for the gas oven show that the electric oven in general has greater work required to remove adhesion. The urethane paints seem to be overall more adhesive for shorter bake times (with the exception of the acrylic paint in the electric oven in CH2I2) but the acrylic paints seem to be more adhesive over a longer bake time. Overall, the acrylic paint and the electric oven seem to be the best. 3. A steel part was painted many years ago. How much of the surface is now covered with paint if the measured water contact angle of the part is 93.4 degrees? The water contact angle of the steel prior to initial painting was 43.8 degrees. After initial painting the contact angle was found to be 114 degrees. ( ) ( ( ) ) What would the paint coverage be if the surface roughness of the painted surface (after the years of use) 1.15? ( ( ) ( ( ( ) ( ) ) ) ( ( ) ( ) ) ( ) ) ( ) Transport Phenomena Test 1. Doctors are studying the different flow rates throughout the human vasculature system. After years of eating fries and hamburgers, four out of ten Americans are obese, and most Americans have a decreased vessel diameter due to fat buildup, increasing the risk of heart attack and stroke. (a) Use Buckingham Pi theory to develop the dimensionless numbers for this system. Representative variables: ρ, P, L, V, μ P V μ L ρ Length Kg/m·s2 m/s Kg/m·s M Kg/m3 Mass Kg/m·s2 Kg/m·s Time Kg/m·s2 m/s Kg/m·s Kg/m3 Kg/m3 5 q’s 3 u’s 2 non-primary q’s (π’s) Choose the π corresponding to: ( ( Kg : 1 – a = 0 a=1 m : -1 + a – b – c = 0 b=1 s : -1 + 2a + c = 0 c = -1 ) ) ( ) ( ) (b) Assume that the growth of fatty deposits on the inside of blood vessels will be limited by the shear stress imposed on the deposit by the flow of blood through the vessel; that is, assume that the growth of fatty deposits on the inside wall of a blood vessel decreases with increasing shear stress τrz. As the deposits grow and the tube narrows, will the growth of fatty deposits slow down over time, or accelerate? Answer this question assuming: (i) constant pressure and (ii) constant flow rate. (i) constant pressure: decelerates due to increased shear stress (τ) with increased speed. Despite keeping higher Cmax, the shear stress causes less growth. (ii) constant flow rate: decelerates since . Since Vx is constant, as dx shrinks (diameter shrinks), the shear stress increases and thus the growth slows. (c) The diameter of the carotid artery, the blood vessel that supplies blood to the brain, is 7 mm, and the average velocity and density of blood is 0.4 m/s and 1060 kg/m3 respectively. Across the blood vessel length of 1m and with a blood viscosity of 0.0027 Pa·s, calculate: (i) the Reynolds number of blood through this healthy vessel; (ii) the friction factor; (iii) the pressure difference across the vessel. d = 0.007 m V = 0.4 m/s ρ = 1060 kg/m3 ( )( )( L=1m µ = 0.0027 Pa·s ) ( ) (d) In one such person, fat has built up on the interior vessel wall over a period of years, restricting blood flow and endangering the person’s life. If there is a 0.75 mm layer of fat on the carotid arterial wall resulting in a decreased vessel radius Rf, what is the new average velocity which gives the same flow rate Q as in part c? ( ( ) ) ( ) 2. It has been proposed that some MEMS (Micro Electro-Mechanical Systems) device parts for high temperature applications could be made out of magnesium oxide by water etching, due to the slight solubility of magnesium oxide in water. The etching reaction is: MgO + H2O → Mg2+ + 2OH− A magnesium oxide plate 5 cm (0.05 m) long partially covered by a polymer etching mask is placed in a water tank near an impeller which generates a free stream water velocity of 1 m/s past the plate. Data: • Mg2+ diffusivity in water: D = 10−5 cm2/s (= 10−9 m2/s ). • Mg2+ solubility in this particular solution: Cs = 10−2 mol/cm3. (a) Sketch the shapes of the momentum and diffusion boundary layers above the plate on one sketch, clearly indicating which of the two boundary layers will be larger. Mg2+ H2O )( ( ( ( 𝑑𝑖𝑓𝑓𝑢𝑠𝑖𝑜𝑛 𝛿 𝑚𝑜𝑚𝑒𝑛𝑡𝑢𝑚 𝛿𝑇 𝑥 ) ) ) 𝑉 𝑥 𝐿 (b) If the magnesium oxide dissolution is limited by mass transfer of Mg2+ ions away from the interface, will the dissolution rate be uniform across the plate? If not, indicate on your sketch from part 2a where on the plate you expect to see the highest and lowest dissolution rates. No, the dissolution rate will not be linear across the plate. The rate will be highest at x=0 and slowest at x=L as shown in the graph below. 𝑥 𝐿 𝑥 (c) Calculate the local Sherwood number Shx at the back end of the plate (x = L). ( )( ) ( ) (d) If the plate were at a different temperature from the fluid, how would the energy transfer boundary layer compare to the momentum and mas transfer boundary layers. The thermal energy boundary barrier is always smaller than both the diffusion and the momentum boundary layers for this system. 3. Two immiscible liquids are flowing in laminar flow between two parallel plates. Is the velocity distribution shown below ever possible? Please explain your answer, assuming that the velocity profile given in the figure is parabolic for both Liquid A and B. Liquid A Liquid B The proposed velocity distribution is not possible. To have the different maximum velocity profiles shown, the faster liquid (B) must have a smaller viscosity than the other liquid (A). On top of that, at the interface of the two liquids, there must be no difference in the shear stress. By which, it can be seen that there should be no difference in the velocity of the two liquids at the interface (as displayed in the diagram). However, since there is no τ change at the interface, the relative τ for liquid A should dictate that liquid A reaches the speed at the boundary equal to the speed of liquid B at the boundary. So liquid A then feels the boundary of liquid B as a faster liquid and thus does not slow to the boundary speed, but instead stays sped up. Liquid B, while meeting the boundary speed, must decrease its maximum speed to match the drag felt by liquid A. Thus, the velocity distribution should instead follow the profile drawn in to the left.
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