Week 4: Project - Steady state simulation of flow over a throttle body

AIM: To Set up and run the steady state simulation for flow over throttle body and to Post process the results

Theoritical Background:

Throttling valves are a type of valve that can be used to start, stop and regulate the flow of fluid through a rotodynamic pump. When the flow of a pump is regulated using a throttling valve, the system curve is changed. The operating point moves to the left on the Pump curve when the flow is decreased

A throttle is the mechanism by which fluid flow is managed by constriction or obstruction. The term throttle refers to any mechanism by which the power or speed of an engine is regulated, such as a car's accelerator pedal.

An engine power can be increased or decreased by the restriction of inlet gases (by the use of a throttle), but usually decreased. Throttle is also called a thrust lever, particularly for jet engine powered aircraft. The throttle pedal or lever acts as a direct linkage. The butterfly valve of the throttle is operated by means of an arm piece, loaded by a spring. This arm is usually directly linked to the accelerator cable, and operates in accordance with the driver, who hits it. The further the pedal is pushed, the wider the throttle valve opens.The throttle body is the part of the air intake system that controls the amount of air flowing into the engine, in response to driver accelerator pedal input in the main. The largest piece inside the throttle body is the throttle plate, which is a butterfly valve that regulates the airflow.

Geometry:

Meshing:

Mesh size is decreased around the throttle, which helps in capturing the results at the boundary of the throttle more accurately and also results in smoothing of the countour around the throttle. This leads to more computational time.

Case Setup:

1. Fluid: Air

Mass fractions of Nitrogen: 0.77, Mass fractions of Oxygen: 0.23

2. Solver: Steady-state Pressure based solver is used to simulate the flow

3. Boundary Conditions:

We have to assign boundary conditions for different faces of Geometry as shown in the table below

4. Regions and Initialization:

Flow region: Volumetric Flow region, Total Pressure: 101325 Pa, Temperature: 300 K, Species : Air

5. Turbulance Model: RNG k-ε.

6. Grid Control: dx=dy=dz=2e-3 m

Fixed embedding - Entity type - Boundary, Boundary ID - Throttle , Mode - Permanent, Scale - 3, Embed layers - 2

Post Processing:

Mass flow rate(kg/s)

Total Pressure(Pa) and Static Pressure(Pa)

Average Velocity(m/s)

Total Cell count

Velocity Contour

The throttle plate and the throttle shaft provides restriction for the flow of intake air. Lesser is the restriction across the flow, lower is the loss of energy. This increases the velocity at the outlet of the throttle body. The velocity at the gap between the Throttle and the wall is high as the pressure at that region is least.

Velocity distribution on the throttle

Velocity vector around the throttle

Velocity Streamlines

Pressure Contour

Pressure distribution on the throttle

Pressure vector around the throttle

Observations:

1. The Mass flow rate takes turbulance initially and converges over the period. The Inflow mass flow rate is balanced with the outflow mass flow rate following the law of conservation of Energy.

2. Throat region has minimum area available for the air to flow. In order to reduce the energy loss, flow gets acclerated at the throat, hence pressure drop at the throat is minimum due to maximum velocity.

3. The Static pressure at the Inlet region drops due to increase in velocity and gets stable as the simulation proceeds. The total pressure increases at the outlet region and converges over a period of time.

4. Equillibrium behaviour of fluids under different boundary conditions can be analysed by the separation of flows. This helps to control the flow behaviour of fluids.