Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

An air cannon uses compressed air to propel a projectile from rest to a final velocity. Consider an air cannon that is to accelerate a 10 -gram projectile to a speed of \(300 \mathrm{m} / \mathrm{s}\) using compressed air, whose temperature cannot exceed \(20^{\circ} \mathrm{C}\) The volume of the storage tank is not to exceed \(0.1 \mathrm{m}^{3} .\) Select the storage volume size and maximum storage pressure that requires the minimum amount of energy to fill the tank.

Short Answer

Expert verified
Answer: The storage volume size that requires the minimum amount of energy to fill the tank is 0.1 m^3, and the maximum storage pressure is approximately 105625 Pa.

Step by step solution

01

Recall Key Equations

In this problem, we need to use the ideal gas law and the conservation of energy. The ideal gas law equation is \(PV=nRT\), where P is the pressure, V is the volume, n is the number of moles of gas, R is the ideal gas constant, and T is the temperature in Kelvin. The conservation of energy equation is \(W = \dfrac{1}{2}mv^2\), where W is the work done, m is the mass of the projectile, and v is the final velocity.
02

Convert Units to SI and Temperature to Kelvin

Convert the mass of the projectile to kilograms and the temperature to Kelvin: m = 10 grams = 0.01 kg, T = 20°C = 293.15 K.
03

Calculate the Work Done and Number of Moles of Gas

Calculate the work done by substituting the given values into the conservation of energy equation: W = (1/2)(0.01 kg)(300 m/s)^2 = 450 J. Then, solve for the number of moles (n) using the ideal gas law, assuming standard pressure of 101325 Pa for the tank when empty: n = (101325 Pa)(0.1 m^3) / (8.314 J/(mol·K)·293.15 K) ≈ 4.127 mol.
04

Determine the Final Pressure

We can calculate the final pressure using the work-energy theorem: W = Δ(PV). Since P_initial * V_initial = P_final * V_final and V_initial = V_final, that means that P_final = P_initial + ΔP or ΔP = P_final - P_initial. So, the work-energy theorem becomes W = V * (P_final - P_initial). Rearranging for P_final, we get P_final = P_initial + (W/V). Substituting known values, we have P_final = 101325 Pa + (450 J / 0.1 m^3) ≈ 105625 Pa.
05

Calculate the Minimum Energy Required

Now we need to minimize the energy required to fill the tank. The energy required is determined by the work done on the gas to increase its pressure. As the volume increases, the amount of work required to compress the gas to achieve the same pressure decreases. Thus, to minimize the energy required, we should use the maximum allowable volume of 0.1 m^3.
06

Provide the Results

The storage volume size that requires the minimum amount of energy to fill the tank is 0.1 m^3, and the maximum storage pressure is approximately 105625 Pa.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Two mass streams of the same ideal gas are mixed in a steady-flow chamber while receiving energy by heat transfer from the surroundings. The mixing process takes place at constant pressure with no work and negligible changes in kinetic and potential energies. Assume the gas has constant specific heats. (a) Determine the expression for the final temperature of the mixture in terms of the rate of heat transfer to the mixing chamber and the inlet and exit mass flow rates. (b) Obtain an expression for the volume flow rate at the exit of the mixing chamber in terms of the volume flow rates of the two inlet streams and the rate of heat transfer to the mixing chamber. (c) For the special case of adiabetic mixing, show that the exit volume flow rate is the sum of the two inlet volume flow rates.

Air at \(300 \mathrm{K}\) and \(100 \mathrm{kPa}\) steadily flows into a hair dryer having electrical work input of \(1500 \mathrm{W}\). Because of the size of the air intake, the inlet velocity of the air is negligible. The air temperature and velocity at the hair dryer exit are \(80^{\circ} \mathrm{C}\) and \(21 \mathrm{m} / \mathrm{s},\) respectively. The flow process is both constant pressure and adiabatic. Assume air has constant specific heats evaluated at \(300 \mathrm{K}\). (a) Determine the air mass flow rate into the hair dryer, in \(\mathrm{kg} / \mathrm{s}\). ( \(b\) ) Determine the air volume flow rate at the hair dryer exit, in \(\mathrm{m}^{3} / \mathrm{s}\).

An air-conditioning system is to be filled from a rigid container that initially contains 5 kg of liquid \(R-134 a\) at \(24^{\circ} \mathrm{C}\). The valve connecting this container to the air-conditioning system is now opened until the mass in the container is \(0.25 \mathrm{kg},\) at which time the valve is closed. During this time, only liquid \(R-134\) a flows from the container. Presuming that the process is isothermal while the valve is open, determine the final quality of the \(R-134 a\) in the container and the total heat transfer.

Refrigerant 134 a enters a compressor with a mass flow rate of \(5 \mathrm{kg} / \mathrm{s}\) and a negligible velocity. The refrigerant enters the compressor as a saturated vapor at \(10^{\circ} \mathrm{C}\) and leaves the compressor at \(1400 \mathrm{kPa}\) with an enthalpy of \(281.39 \mathrm{kJ} / \mathrm{kg}\) and a velocity of \(50 \mathrm{m} / \mathrm{s}\). The rate of work done on the refrigerant is measured to be \(132.4 \mathrm{kW}\). If the elevation change between the compressor inlet and exit is negligible, determine the rate of heat transfer associated with this process, in \(\mathrm{kW}\).

In a single-flash geothermal power plant, geothermal water enters the flash chamber (a throttling valve) at \(230^{\circ} \mathrm{C}\) as a saturated liquid at a rate of \(50 \mathrm{kg} / \mathrm{s}\). The steam resulting from the flashing process enters a turbine and leaves at \(20 \mathrm{kPa}\) with a moisture content of 5 percent. Determine the temperature of the steam after the flashing process and the power output from the turbine if the pressure of the steam at the exit of the flash chamber is \((a) 1 \mathrm{MPa},(b) 500 \mathrm{kPa}\) \((c) 100 \mathrm{kPa},(d) 50 \mathrm{kPa}\).

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free