/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 76 Liquid \(n\) -pentane at \(25^{\... [FREE SOLUTION] | 91Ó°ÊÓ

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Liquid \(n\) -pentane at \(25^{\circ} \mathrm{C}\) is burned with \(30 \%\) excess oxygen (not air) fed at \(75^{\circ} \mathrm{C}\). The adiabatic flame temperature is \(T_{\mathrm{ad}}\left(^{\circ} \mathrm{C}\right)\) (a) Take as a basis of calculation \(1.00 \mathrm{mol} \mathrm{C}_{5} \mathrm{H}_{12}(1)\) burned and use an energy balance on the adiabatic reactor to derive an equation of the form \(f\left(T_{\mathrm{ad}}\right)=0,\) where \(f\left(T_{\mathrm{ad}}\right)\) is a fourth-order polynomial \(\left[f\left(T_{\mathrm{ad}}\right)=c_{0}+c_{1} T_{\mathrm{ad}}+c_{2} T_{\mathrm{ad}}^{2}+c_{3} T_{\mathrm{ad}}^{3}+c_{4} T_{\mathrm{ad} \mathrm{d}}^{4}\right]\). If your derivation is correct, the ratio \(c_{0} / c_{4}\) should equal \(-6.892 \times 10^{14} .\) Use a spreadsheet program to determine \(T_{\mathrm{ad}}\) (b) Repeat the calculation of Part (a) using successively the first two terms, the first three terms, and the first four terms of the fourth-order polynomial equation. If the solution of Part (a) is taken to be exact, what percentage errors are associated with the linear (two-term), quadratic (three-term), and cubic (four-term) approximations? (c) Why is the fourth-order solution at best an approximation and quite possibly a poor one? (Hint: Examine the conditions of applicability of the heat capacity formulas in Table B.2.)

Short Answer

Expert verified
The solution involves determining the adiabatic flame temperature using energy balance with fourth order polynomial approximation. Then, calculating the percentage of errors associated with the linear, quadratic, and cubic approximations by referring the approximated solutions against the result from part (a) which is calculated using all four terms. Lastly, understanding why the fourth-order solution is just an approximation.

Step by step solution

01

Write Complete Combustion Reaction

Write down the combustion reaction \(C_{5}H_{12}(l) + aO_{2}(g) + bN_{2}(g) \rightarrow xCO_{2}(g) + yH_{2}O(l) + cN_{2}(g) + Heat\). Balancing this equation gives \(C_{5}H_{12}(l) + (30/100)* 15/2 O_{2} \rightarrow 5CO_{2} + 6H_{2}O+ Heat\). Assume complete combustion, so \(a=19.5\) and \(b=0\) (no nitrogen as excess oxygen is used not air) and \(x=5\), \(y=6\) and \(c=0\).
02

Establish Energy Balance Equation

Establish the energy balance equation for the adiabatic reactor, which is \(\displaystyle∑H_{reactants}(T_{ref}) -∑H_{products}(T_{ad}) = 0\). Assume temperature of reactants is \(T_{ref} = 25^{\circ} C\) and Flame temperature is \(T_{ad}\). Substitute the enthalpy terms by their respective heat capacities to convert them to temperature dependant.
03

Identify Polynomial

This equation transforms into a fourth-order polynomial \(f(T_{ad}) = c_{0}+c_{1}T_{ad}+c_{2}T_{ad}^{2}+c_{3}T_{ad}^{3}+c_{4}T_{ad}^{4}=0\). Substitute data from Table B.2 to find the coefficients \(c_{0}, c_{1}, c_{2}, c_{3}, c_{4}\). The ratio \(c_{0}/c_{4}\) should be \(-6.892x10^{14}\)
04

Solve Polynomial to find Flame Temperature

Use a spreadsheet program or any polynomial solver to determine \(T_{ad}\) by solving \(f(T_{ad}) = 0\).
05

Repeat Calculation to Determine Errors

Repeat the calculation for only first two terms, then three terms, and then four terms of the polynomial equation. Calculate the percentage of errors associated with the linear (two-term), quadratic (three-term), and cubic (four-term) approximations by considering the result from part(a) with all terms as the exact solution.
06

Analyze Fourth Order Solution

Analyze why the fourth-order solution at best is an approximation and possibly a poor one. This can be done by examining the conditions of applicability of the heat capacity formulas in Table B.2 or understanding that such polynomial equations give only approximations and any initial conditions or assumptions made affect the accuracy.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Combustion Reaction
When understanding adiabatic flame temperature, it’s crucial to begin with the concept of a combustion reaction. Combustion reactions entail the burning of a substance, usually a hydrocarbon, in the presence of an oxidant, generally oxygen. For pentane, a hydrocarbon, the reaction follows:

\[ C_{5}H_{12}(l) + ext{oxygen} ightarrow ext{carbon dioxide} + ext{water} + ext{heat} \]In a perfect or complete combustion, all fuel combines with the oxidant without leaving any residual unburned fuel or oxygen. This yields carbon dioxide (\(CO_2\)) and water (\(H_2O\)), as illustrated by the simplified reaction:
  • \(C_{5}H_{12}(l) + aO_{2}(g) \rightarrow 5CO_{2}(g) + 6H_{2}O(l) + ext{Heat}\)
  • Here, \(aO_{2}\) is calculated based on stoichiometry and the condition that there's 30% excess oxygen.
Balancing the reaction is pivotal to ensure the stoichiometric ratios of fuel to oxidant are correct, influencing the energy calculations and ultimately the adiabatic flame temperature.
Energy Balance Equation
The crux of determining the adiabatic flame temperature is the energy balance equation. For an adiabatic process, where no heat is lost to the surroundings, the principle of conservation of energy applies. The total enthalpy of reactants must equal the total enthalpy of products:\[ \ ∑H_{reactants}(T_{ref}) = ∑H_{products}(T_{ad}) \ \]Where:
  • \(∑H_{reactants}(T_{ref})\) is the initial enthalpy of reactants at the reference temperature, typically seen as \(25^{\circ} C\).
  • \(T_{ad}\) represents the adiabatic flame temperature.
For practical calculations, we express enthalpy changes with heat capacity formulas, making adjustments as temperatures change, thus making them temperature-dependent equations. This transformation leads naturally to a polynomial that you can solve for \(T_{ad}\). By maintaining an energy balance, we ensure that combustion efficiency and energy conversions are correctly assessed, lending accuracy to adiabatic flame temperature estimation.
Fourth-Order Polynomial
The polynomial equation representing the energy balance is usually a fourth-order polynomial as seen in combustion calculations:
  • \(f(T_{ad}) = c_{0} + c_{1}T_{ad} + c_{2}T_{ad}^{2} + c_{3}T_{ad}^{3} + c_{4}T_{ad}^{4} = 0 \)
This mathematical approach mirrors how changes in temperature affect reaction thermodynamics. Coefficients \(c_{0}\) through \(c_{4}\) are calculated using data, like calorific capacity samples from reference materials (e.g., Table B.2 in our exercise). By setting up this polynomial, we're using both the known quantities and molecular energy estimations to solve for \(T_{ad}\), where the root of the polynomial gives the flame temperature.However, approximating through such polynomials always introduces slight inaccuracies because real-world conditions rarely align perfectly with theoretical calculations.
Heat Capacity Formulas
The role of heat capacity formulas in the energy balance cannot be overstated. Heat capacity indicates how much heat a substance can store as it changes temperature. As temperatures in reactions vary, heat capacity helps to assess energy changes over that range.For instance, to convert enthalpies into temperature related values, formulas for specific heat capacities \( C_{p} \) are used:
  • These formulas typically vary with temperature, often expressed in the polynomial form \(C_{p} = A + BT + CT^{2} + ...\).
  • Dependence of \(C_{p}\) on temperature means these coefficients must be precise to ensure accurate energy calculation.
Neglecting these variabilities or misapplying conditions can cause significant errors. Subtle temperature changes or assumptions in heat capacity's temperature dependency might make a fourth-order polynomial less responsive to abrupt or irregular conditions, and this is why calculated results, though close, remain approximations.

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Most popular questions from this chapter

Formaldehyde is produced commercially by the catalytic oxidation of methanol. In a side reaction, methanol is oxidized to \(\mathrm{CO}_{2}\) $$\begin{array}{l}\mathrm{CH}_{3} \mathrm{OH}+\mathrm{O}_{2} \rightarrow \mathrm{CH}_{2} \mathrm{O}+\mathrm{H}_{2} \mathrm{O} \\\\\mathrm{CH}_{3} \mathrm{OH}+\mathrm{O}_{2} \rightarrow \mathrm{CO}_{2}+2 \mathrm{H}_{2} \mathrm{O}\end{array}$$ A mixture containing 55.6 mole \(\%\) methanol and the balance oxygen enters a reactor at \(350^{\circ} \mathrm{C}\) and \(1 \mathrm{atm}\) at a rate of \(4.60 \times 10^{4} \mathrm{L} / \mathrm{s}\). The reaction products emerge at the same temperature and pressure at a rate of \(6.26 \times 10^{4} \mathrm{L} / \mathrm{s} .\) An analysis of the products yields a molar composition of \(36.7 \% \mathrm{CH}_{2} \mathrm{O}, 4.1 \% \mathrm{CO}_{2}\) \(14.3 \% \mathrm{O}_{2},\) and \(44.9 \% \mathrm{H}_{2} \mathrm{O} .\) The required reactor cooling rate is calculated to be \(1.05 \times 10^{5} \mathrm{kW}\) (a) Is the calculated cooling rate correct for the given stream data? (b) The stream data cannot be correct. Prove it.

A gaseous fuel containing methane and ethane is burned with excess air. The fuel enters the furnace at \(25^{\circ} \mathrm{C}\) and 1 atm, and the air enters at \(200^{\circ} \mathrm{C}\) and 1 atm. The stack gas leaves the furnace at \(800^{\circ} \mathrm{C}\) and 1 atm and contains 5.32 mole\% \(\mathrm{CO}_{2}, 1.60 \%\) CO, \(7.32 \%\) O \(_{2}, 12.24 \% \mathrm{H}_{2} \mathrm{O}\), and the balance \(\mathrm{N}_{2}\). (a) Calculate the molar percentages of methane and ethane in the fuel gas and the percentage excess air fed to the reactor. (b) Calculate the heat (kJ) transferred from the reactor per cubic meter of fuel gas fed. (c) A proposal has been made to lower the feed rate of air to the furnace. State advantages and a drawback of doing so.

Sulfur dioxide is oxidized to sulfur trioxide in a small pilot-plant reactor. SO \(_{2}\) and \(100 \%\) excess air are fed to the reactor at \(450^{\circ} \mathrm{C}\). The reaction proceeds to a \(65 \% \mathrm{SO}_{2}\) conversion, and the products emerge from the reactor at \(550^{\circ} \mathrm{C}\). The production rate of \(\mathrm{SO}_{3}\) is \(1.00 \times 10^{2} \mathrm{kg} / \mathrm{min}\). The reactor is surrounded by a water jacket into which water at \(25^{\circ} \mathrm{C}\) is fed. (a) Calculate the feed rates (standard cubic meters per second) of the \(\mathrm{SO}_{2}\) and air feed streams and the extent of reaction, \(\xi\) (b) Calculate the standard heat of the SO_ oxidation reaction, \(\Delta H_{\mathrm{t}}^{\mathrm{r}}(\mathrm{kJ}) .\) Then, taking molecular species at \(25^{\circ} \mathrm{C}\) as references, prepare and fill in an inlet-outlet enthalpy table and write an energy balance to calculate the necessary rate of heat transfer ( \(\mathrm{kW}\) ) from the reactor to the cooling water. (c) Calculate the minimum flow rate of the cooling water if its temperature rise is to be kept below \(15^{\circ} \mathrm{C}\) (d) Briefly state what would have been different in your calculations and results if you had taken elemental species as references in Part (b).

Formaldehyde is produced by decomposing methanol over a silver catalyst: $$\mathrm{CH}_{3} \mathrm{OH} \rightarrow \mathrm{HCHO}+\mathrm{H}_{2}$$ To provide heat for this endothermic reaction, some oxygen is included in the feed to the reactor, leading to the partial combustion of the hydrogen produced in the methanol decomposition. The feed to an adiabatic formaldehyde production reactor is obtained by bubbling a stream of air at 1 atm through liquid methanol. The air leaves the vaporizer saturated with methanol and contains \(42 \%\)methanol by volume. The stream then passes through a heater in which its temperature is raised to \(145^{\circ} \mathrm{C} .\) To avoid deactivating the catalyst, the maximum temperature attained in the reactor must be limited to \(600^{\circ} \mathrm{C}\). For this purpose, saturated steam at \(145^{\circ} \mathrm{C}\) is metered into the air-methanol stream, and the combined stream cnters the reactor. A fractional methanol conversion of \(70.0 \%\) is achicved in the reactor, and the product gas contains 5.00 mole\% hydrogen. The product gas is cooled to \(145^{\circ} \mathrm{C}\) in a waste heat boiler in which saturated steam at 3.1 bar is generated from liquid water at \(30^{\circ} \mathrm{C}\). Several absorption and distillation units follow the waste heat boiler, and formaldehyde is ultimately recovered in an aqueous solution containing 37.0 wt\% HCHO. The plant is designed to produce 36 metric kilotons of this solution per year, operating 350 days/yr. (a) Draw the process flowchart and label it completely. Show the absorption/distillation train as a single unit with the reactor product gas and additional water entering and the formaldehyde solution and a gas stream containing methanol, oxygen, nitrogen, and hydrogen leaving. (b) Calculate the operating temperature of the methanol vaporizer. (c) Calculate the required feed rate of steam to the reactor \((\mathrm{kg} / \mathrm{h})\) and the molar flow rate and composition of the product gas. (d) Calculate the rate ( \(\mathrm{kg} / \mathrm{h}\) ) at which steam is generated in the waste heat boiler. (e) Enough saturated steam was added to the feed to the reactor to keep the reactor outlet temperature at \(600^{\circ} \mathrm{C}\). Explain in your own words (i) why adding steam lowers the outlet temperature, and (ii) the cconomic drawbacks of higher and lower outlet temperatures.

A mixture of air and a fine spray of gasoline at ambient (outside air) temperature is fed to a set of pistonfitted cylinders in an automobile engine. Sparks ignite the combustible mixtures in one cylinder after another, and the consequent rapid increase in temperature in the cylinders causes the combustion products to expand and drive the pistons. The back-and-forth motion of the pistons is converted to rotary motion of a crank shaft, motion that in turn is transmitted through a system of shafts and gears to propel the car. Consider a car driving on a day when the ambient temperature is 298 K and suppose that the rate of heat loss from the engine to the outside air is given by the formula $$-\dot{Q}_{1}\left(\frac{\mathrm{kJ}}{\mathrm{h}}\right) \approx \frac{15 \times 10^{6}}{T_{\mathrm{a}}(\mathrm{K})}$$ where \(T_{\mathrm{a}}\) is the ambient temperature. (a) Take gasoline to be a liquid with a specific gravity of 0.70 and a higher heating value of \(49.0 \mathrm{kJ} / \mathrm{g}\), assume complete combustion and that the combustion products leaving the engine are at \(298 \mathrm{K}\), and calculate the minimum feed rate of gasoline (gal/h) required to produce 100 hp of shaft work. (b) If the exhaust gases are well above \(298 \mathrm{K}\) (which they are), is the work delivered by the pistons more or less than the value determined in Part (a)? Explain. (c) If the ambicnt temperature is much lower than \(298 \mathrm{K}\), the work delivered by the pistons would decrease. Give two reasons.

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