Mass flow rate equation thermodynamics

Mass flow rate equation thermodynamics

The conservation of mass is a fundamental concept of physics. Within some problem domain, the amount of mass remains constant --mass is neither created nor destroyed. The mass of any object is simply the volume that the object occupies times the density of the object.

For a fluid a liquid or a gas the density, volume, and shape of the object can all change within the domain with time. And mass can move through the domain. On the figure, we show a flow of gas through a constricted tube. There is no accumulation or destruction of mass through the tube; the same amount of mass leaves the tube as enters the tube.

At any plane perpendicular to the center line of the tube, the same amount of mass passes through. We call the amount of mass passing through a plane the mass flow rate.

The conservation of mass continuity tells us that the mass flow rate through a tube is a constant. We can determine the value of the mass flow rate from the flow conditions. If the fluid initially passes through an area A at velocity Vwe can define a volume of mass to be swept out in some amount of time t. The volume v is:. The mass m contained in this volume is simply density r times the volume.

mass flow rate equation thermodynamics

To determine the mass flow rate mdotwe divide the mass by the time. The resulting definition of mass flow rate is shown on the slide in red. How do engineers use this knowledge of the mass flow rate?

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From Newton's Second Law of Motion, the aerodynamic forces on an aircraft lift and drag are directly related to the change in momentum of a gas with time. The momentum is defined to be the mass times the velocity, so we would expect the aerodynamic forces to depend on the mass flow rate past an object.

The thrust produced by a propulsion system also depends on the change of momentum of a working gas.

Mass Flow Rate, Volume Flow Rate, Velocity and Cross Sectional Area

The thrust depends directly on the mass flow rate through the propulsion system. For flow in a tube, the mass flow rate is a constant. For a constant density flow, if we can determine or set the velocity at some known area, the equation tells us the value of velocity for any other area.

If we desire a certain velocity, we know the area we have to provide to obtain that velocity.The mass flow rate is defined as the amount of mass flowing through a cross-section per unit time. The flow rate through a differential area dA is:. Normal Velocity Component. The volume flow rate is the volume of the fluid flowing through a cross-sectional area per unit time. System Used for Conservation of Mass Equation. Mass Remains Constant for a Closed System A closed system is defined as a system which mass can not cross its boundaries, but energy transfer is allowed.

Since no mass flows in or out of the system, the mass of the closed system remains constant during a process. Net mass transfer to or from a system during a process is equal to the net change in the total mass of the system during that process.

First Law of Thermodynamics. Multimedia Engineering Thermodynamics. Conservation of Mass. Conservation of Energy. Solids and Liquids. Ideal Gas. Case Intro. Case Solution. Pure Substances. First Law. Energy Analysis. Second Law. Exergy Analysis. Gas Power Cyc.

Brayton Cycle. Rankine Cycle. Basic Math.

mass flow rate equation thermodynamics

Thermo Tables. Mass Flow Rate Through a Duct. Integrating the above equation to get the total mass flow rate. The mass and volume flow rate are related by.Close this panel. Equations for Determing the Mass Flow Rate. Therefore, the mass flow rate can be deteremined from:.

Lesson 5A Blog. Confused and have questions? We've got answers. With Chegg Studyyou can get step-by-step solutions to your questions from an expert in the field. If you rather get study help, try 30 minutes of free online tutoring with Chegg Tutors.

All rights reserved. Roll your mouse over this box to close. B in the LT Blog day membership. LT A Benefits. Log-In to LT A. Density is just the ratio of the mass of a chunk of fluid to its volume. The cool part is that the density is also the ratio of the mass flow rate to the volumetric flow rate. Volumetric flow rate is a new idea, but not a scary one. It is a common way to express a flow rate. Another way to look at this relationship is to say that the mass flow rate of a stream is the product of the volumetric flow rate and the density.

It is fine to use density in this equation, but in this course we usually think in terms of the specific volume, which the inverse of the density. This is the tricky part. The volumetric flow rate is the integral of the velocity over the circular cross-sectional area through which the fluid flows. That is, the integral of v dA.

The easiest differential area to use when integrating over a circular area is a ring.Fortunately we will be able to separately analyse each component of the system independent of the entire system, which is typically represented as follows:. In addition to the energy flow across the control volume boundary in the form of heat and work, we will also have mass flowing into and out of the control volume.

We will only consider Steady Flow conditions throughout, in which there is no energy or mass accumulation in the control volume, thus we will find it convenient to derive the energy equation in terms of power [kW] rather than energy [kJ].

Furthermore the term Control Volume indicates that there is no boundary work done by the system, and typically we have shaft work, such as with a turbine, compressor or pump. Consider an elemental mass d m flowing through an inlet or outlet port of a control volume, having an area A, volume d V, length d x, and an average steady velocityas follows. Thus finally the mass flow rate can be determined as follows:. The fluid mass flows through the inlet and exit ports of the control volume accompanied by its energy.

These include four types of energy - internal energy ukinetic enegy kepotential energy peand flow work w flow. In order to evaluate the flow work consider the following exit port schematic showing the fluid doing work against the surroundings through an imaginary piston:.

It is of interest that the specific flow work is simply defined by the pressure P multiplied by the specific volume v. In the following section we can now develop the complete energy equation for a control volume. Consider the control volume shown in the following figure. Under steady flow conditions there is no mass or energy accumulation in the control volume thus the mass flow rate applies both to the inlet and outlet ports.

Furthermore with a constant mass flow rate, it is more convenient to develop the energy equation in terms of power [kW] rather than energy [kJ] as was done previously. The total power in due to heat and mass flow through the inlet port 1 must equal the total power out due to work and mass flow through the outlet port 2thus:. The specific energy e can include kinetic and potential energy, however will always include the combination of internal energy u and flow work Pvthus we conveniently combine these properties in terms of the property enthalpy as was done in Chapter 3aas follows:.

Note that z is the height of the port above some datum level [m] and g is the acceleration due to gravity [9. Substituting for energy e in the above energy equation and simplifying, we obtain the final form of the energy equation for a single-inlet single-outlet steady flow control volume as follows:. Notice that enthalpy h is fundamental to the energy equation for a control volume.

When dealing with closed systems we found that sketching T-v or P-v diagrams was a significant aid in describing and understanding the various processes.

In steady flow systems we find that the Pressure-Enthalpy P-h diagrams serve a similar purpose, and we will use them extensively. In this course we consider three pure fluids - water, refrigerant Ra, and carbon dioxide, and we have provided P-h diagrams for all three in the Property Tables section.

We will illustrate their use in the following examples. The P-h diagram for water is shown below. Study it carefully and try to understand the significance of the distinctive shapes of the constant temperature curves in the compressed liquid, saturated mixture quality region and superheated vapor regions.A text only version of this slide is available which gives all of the flow equations.

The interactive Java applet EngineSim is also available. This program solves these equations and displays the thrust and fuel flow values for a variety of turbine engines. The propulsion system of an aircraft must perform two important roles:. On this page we show the thermodynamic equations which relate the the temperature ratio in the burner to the fuel mass flow rate. The fuel mass flow rate is related to the total engine air flow rate mdot a by the fuel to air ratio f.

The energy equation for the burner can be solved for the temperature ratio across the burner:. Using the temperature equation, and a little algebra, it is possible to solve for the fuel to air ratio f. From the fuel to air ratio, we can obtain the fuel mass flow rate by a simple multiplication.

The engine air flow rate is normally set by conditions in the nozzle. We can use the value of fuel to air ratio to determine the engine's specific fuel consumption. As explained in another section of the Beginner's Guide to Aerodynamics, the specific fuel consumption and the aircraft fuel load determine the maximum flight time and the maximum range of an aircraft.

If we try to run the engine hotter than this maximum temperature, the burner and the turbine will be damaged. You can now use EngineSim to study the effects of different materials on engine operation. Back to top.In this article we will discuss about:- 1. Introduction to First Law of Thermodynamics 2. Energy — A Property of the System 4. Different Forms of Stored Energies 5. Adiabatic Index 7.

Energy is inherent in all matters. Energy may appear in many different forms. Conversion can be made from one form of energy to another. We are unable to define the general term energy in a simple way, but we can define with precision the various forms in which it appears. Except the nuclear reaction, where mass is converted into energy total energy of the universe is constant. For this matter, First Law of Thermodynamics can be expressed as—.

Energy can neither be created nor destroyed except in nuclear reactions. This is the law of conservation of energy. First Law for a Closed System Undergoing a Process : If a closed system undergoes a change of state or a process and during which, both work transfer and heat transfer are involved, then the net energy transfer will be stored within the system.

If Q is the amount of heat transferred to the system and W is the amount of work transferred from the system, during the process, and then the net energy transfer Q — W will be stored in the system. Energy in storage is neither heat nor work, but is called as Internal energy or simply energy of the system. Energy — A Property of the System: Consider a system which changes its state from state 1 to state 2 by following the path A, and returns from state 2 to state 1 by following the path B as shown in Fig.

So the system undergoes a cycle. Now writing the I-law for the path A. Thus the change in energy for the path B and C are same. Hence change in energy does not depend upon path, so it depends on end states. Hence, it is a point function and since properties are point functions, Energy is a property of the system.Documentation Help Center Documentation. The Control Volume System block models a constant volume open thermodynamic system with heat transfer.

The block uses the conservation of mass and energy, assuming an ideal gas, to determine the pressure and temperature. The block implements an automotive-specific Constant Volume Pneumatic Chamber block that includes thermal effects related to the under hood of passenger vehicles. You can specify heat transfer models:. You can use the Control Volume System block to represent engine components that contain volume, including pipes and manifolds. The Control Volume System block implements a constant volume chamber containing an ideal gas.

To determine the rate changes in temperature and pressure, the block uses the continuity equation and the first law of thermodynamics.

mass flow rate equation thermodynamics

The Control Volume Source block is part of a flow network. Blocks in the network determine the mass fractions that the block will track during simulation.

Mass flow rate

The block can track these mass fractions:. Using the conservation of mass for each gas constituent, this equation determines the rate change:. To calculate the heat transfer, you can configure the Control Volume Source block to calculate the heat transfer across the wall of the control volume.

The block determines the interior convection heat transfer coefficient using a lookup table that is a function of the average mass flow rate. For the power accounting, the block implements these equation based on the number of inlet and outlet ports. PwrNotTrnsfrd — Power crossing the block boundary, but not transferred. For example, if you configure your block with 3 input ports and 2 outlet ports, the block implements these equations.

To create input ports, specify the Number of inlet ports parameter. To create this port, select External input for the Heat transfer model parameter. To create this port, select External wall convection for the Heat transfer model parameter. Nitric oxide and nitrogen dioxide mass fraction. Port i heat flow. To create outlet ports, specify the Number of outlet ports parameter.

Selecting Constant or External wall convection enables the Heat Transfer parameters. Initial chamber pressure, P volin Pa.

Initial chamber temperature, T volin K. To enable this parameter, select Constant for the Heat transfer model parameter. To enable this parameter, select External wall convection for the Heat transfer model parameter.

mass flow rate equation thermodynamics

Initial mass temperature, T massin K. Simulate a full vehicle model with an internal combustion engine, transmission, and associated powertrain control algorithms. Use for powertrain matching analysis and component selection, control and diagnostic algorithm design, and hardware-in-the-loop HIL testing.

Internal Combustion Engine Fundamentals.

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