Compressible Flow CFD Simulation Training Package, Advanced Users, 10 Projects
$633.00 Student Discount
This CFD training package is prepared for ADVANCED users of ANSYS Fluent software in the COMPRESSIBLE FLOW area including 10 practical exercises.
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Description
Compressible Flow CFD Simulation Package, 10 ANSYS Fluent Training for ADVANCED Users
This CFD training package is prepared for ADVANCED users of ANSYS Fluent software in the COMPRESSIBLE FLOW area including 10 practical exercises. You will learn and obtain comprehensive training on how to simulate projects. The achieved knowledge will enable you to choose the most appropriate modeling approaches and methods for applications and CFD simulations.
Compressible Flow occurs in many industrial devices and applications. some of these cases are investigated in this training package.
Compressor
Problem 1 simulates the air compression inside a Rampressor. The rampressor is a unique type of ultrasonic compressor rotor that operates at a high-pressure ratio, and engine technology and gas compression are the ramjet ultrasonic shock wave. The operating mechanism of these compressors is such that the gas flow passes through a fixed outer cover and a sloping surface or inner ramp.
Aerial Structure
Problem 2 simulates compressible flow around an aerial structure considering Large Eddy Simulation (LES). A density-based approach has been used to define the type of airflow solution around this aerial structure; Because the existing airflow is entirely compressible.
Project 3, supersonic flow over an F-16 aircraft considering inviscid fluid was simulated, and then the results were investigated. Supersonic speed is the speed of an object that exceeds the speed of sound. It is estimated to be around 343 m/s in the dry air at a temperature of 20 C.
Car
In Project 4, the aerodynamic coefficients of a Formula One (F1) car by two different solvers pressure-based and density-based, have been studied, at a speed of 108 meters per second at a lateral angle of zero degrees (actually a straight path). This velocity at the ground level is equivalent to a Mach number of approximately 0.32. We know this area from Mach number is the transition zone from incompressible to compressible flow, so on this geometry, the drag coefficient is investigated using two pressure-based and density-based solvers is discussed.
Steam Ejector
Problem 5 simulates the process of condensation inside a steam ejector. When the Wet Steam multiphase model is used, two sets of transport equations are solved: the mass fraction of the condensed liquid phase and the number or concentration of droplets per unit volume.
Paper Numerical Validation in Compressible Flow CFD Simulation Training Package
NACA0012
In project 6, we simulated the compressible flow around the NACA0012 airfoil, and then we compare the results with the results extracted from an article called this “Numerical Simulation OF VISCOUS TRANSONIC AIRFOIL FLOWS”.
Steam Ejector
Problem 7 simulates the water vapor flow inside a steam ejector. This numerical simulation is based on the reference paper “CFD simulation on the effect of primary nozzle geometries for a steam ejector in refrigeration cycle” and the results of the present numerical work are compared and validated with the results in the reference article. An ejector is a mechanical device that uses an actuator fluid to suck a secondary material (gas, liquid, or solid particles), and finally, the actuator fluid and the suction substance are mixed together and exit from the system.
Turbine Cascade
Problem 8 simulates the two-dimensional compressible flow field through a transonic linear turbine cascade. The present project’s results are compared with the experimental results of the paper “Midspan Flow-Field Measurements for Two Transonic Linear Turbine Cascades at Off-Design Conditions”. Turbulence modeling and Computational procedures (boundary conditions, etc.) are simulated based on the article “Numerical study of the flow field through a transonic linear turbine cascade at design and off-design conditions”.
Acoustic in Compressible Flow CFD Simulation Training Package
Problem 9 simulates the acoustic wave and the sound produced inside a Turbojet. The model includes a turbojet that has a fan in its inlet. This fan is rotating at 2000 rpm and around the X-axis in the current model.
RBF Morph
Finally, in Project 10, the flow inside a NACA0012 airfoil is first has been simulated. The angle of attack is 1.53 degrees and the simulation has been done by the density-based solver due to the compressibility with a Mach number equal to 0.7. Then the geometry is optimized to improve lift-to-drag (L/D) as aerodynamic efficiency.
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Call On WhatsApp
Mr. Daryl Kessler –
I’m an advanced user and I’m particularly interested in the underlying physics of the models used in the CFD simulations. Could you explain more about the fundamental principles that these models are based on?
MR CFD Support –
In our Compressible Flow Ansys Fluent Training Package, we use models based on fundamental principles of fluid dynamics. These principles include the conservation of mass, momentum, and energy, which are embodied in the Navier-Stokes equations. The models also incorporate the concept of compressibility, which is essential for accurately simulating high-speed flows. Each exercise in the package provides a deep dive into these principles, allowing advanced users to gain a thorough understanding of the physics involved.
Ima Grant DDS –
I have a specific project in mind that involves complex compressible flow simulations. Can the training package be tailored to suit my specific needs?
MR CFD Support –
Absolutely! At MR-CFD, we understand that every user has unique needs and we’re more than willing to accommodate them. If you have a specific simulation or project in mind, we can customize the training package to suit your requirements. Just let us know what you need, and we’ll do our best to assist you.
Kari Steuber –
I’ve noticed that the training package includes 10 practical exercises. Could you elaborate on the complexity of these exercises and how they can help me in understanding the nuances of compressible flow simulations?
MR CFD Support –
The 10 exercises included in the package are designed to challenge and engage advanced users. They cover a wide range of topics related to compressible flow, including shock waves, supersonic flow, and heat transfer in high-speed flows. Each exercise provides a step-by-step guide to setting up, running, and analyzing a simulation, helping users to gain a deep understanding of the complexities involved in compressible flow simulations.