CFD of External Aerodynamics and Turbomachinery

BY
Udemy

Mode

Online

Fees

₹ 2699

Quick Facts

particular details
Medium of instructions English
Mode of learning Self study
Mode of Delivery Video and Text Based

Course and certificate fees

Fees information
₹ 2,699
certificate availability

Yes

certificate providing authority

Udemy

The syllabus

Introduction to Course

  • Course Introduction

Problem Description of workshop on missile

  • Introduction
  • Boundary layer, first cell height and Y+

Geometry processing in Spaceclaim

  • Opening Spaceclaim and important commands
  • Importing cad model and changing display properties of geometry
  • Cleaning geometry, re-creation of important surfaces and making solids
  • Creating final missile model with fins as single part
  • Fluid domain creation and saving file

Workshop 2 : Tetra Prism Mesh Generation in ICEM CFD

  • Introduction, opening ICEMCFD, Working directory and surface resolution
  • Creating Parts for boundary conditions
  • Mesh settings and volue mesh generation using Octree method
  • Improving surface mesh quality using laplace smoothing
  • Creating density boxes and delaunay mesh
  • Problem Description
  • Prism mesh generation and editing
  • Mesh info and mesh export for Fluent and CFX

Workshop 3 : Problem setup, solution and post processing in Fluent for Missile

  • Opening mesh file, material properties, turbulence model and mesh units&quality
  • Boundary conditions, solution settings and running case
  • Post processing results and mesh adaptation for shock wave resolution

Introduction and problem description for workshop 6, 7& 8

  • Introduction and problem description for workshop 6, 7& 8

Workshop 6a : Centrifugal Fan - Creating Assembly

  • Aligning Fan rotor and inlet cone
  • Aligning Scroll with Fan rotor & Inlet cone
  • Some advanced features of assembly creation in spaceclaim

Workshop 6b : Creating Centrifugal Fan CFD Model in Spaceclaim for iges model

  • Importing IGES file and applying some preliminary settings
  • Moving file to origin, deleting interface region and creating lines
  • Recreating important surfaces
  • Separating different components and some processing
  • Creating final model of scroll with extended region at outlet
  • Creating final model of Inlet-Cone with extended region at inlet
  • Creating final model of centrifugal fan impeller

Workshop 7 : Tetra - Prism Meshing of Centrifugal Fan

  • Introduction and file import into ICEMCFD
  • Creating Tetra-Prism mesh for Inlet-Cone and export in fluent format with BCs
  • Creating Tetra-Prism mesh for Volute/Scroll : Build topology and parts
  • Creating Tetra-Prism mesh for Volute/Scroll : Mesh generation and export
  • Creating Tetra-Prism mesh for centrifugal fan impeller

Turbomachinery CFD Modelling in Fluent

  • Introduction and discussion about SRF and MRF
  • When to use MRF?
  • Setting up SRF model in Fluent
  • Setting up Frozen Rotor model in Fluent and mesh interfaces
  • Setting up mixing plane model in Fluent
  • Setting up sliding mesh model in Fluent
  • Boundary conditions for rotating and stationary domains
  • Summary of different turbomachinery models in Fluent
  • Difference between Frozen rotor, mixing plane and sliding mesh model
  • Best practices for different type of simulation cases

Workshop 8 : Frozen Rotor Analysis of Centrifugal Fan in Fluent

  • Launching fluent and Importing three domain mesh files using append command
  • Setting up interfaces and Frozen Rotor model
  • Turbulence model, near wall treatment, boundary layer and Y+
  • Y+ contours for SST and K-Epsilon realizable model with scalable wall functions
  • Boundary condition
  • Solution methods & controls, residuals & monitors and solution
  • Basic post processing of centrifugal fan : Contours, Vectors and Pathlines
  • Generating Fan performance map - Advanced level post processing
  • Creating solution animation

Workshop 9 : Ahmed Body CFD - Problem Description and important details

  • Introduction to Ahmed Body workshop series
  • Objectives of this workshop
  • Problem description and geometry details
  • Domain dimensions and general discussion of results and settings

Workshop 9 : Ahmed Body geometry generation in design modeler

  • Introduction
  • Starting workbench and design modeler
  • 3_Ahmed body Sketch with all dimensions
  • 3D model generation using extrude command
  • Adding 4 legs using extrude and pattern commands
  • Round, unite and rotate body to required location
  • Creating domain for Ahmed body, symmetric model and removal of legs
  • Creating named selection for boundary conditions
  • Project and geometry open, save in different formats

Workshop 9 : Geometry editing of Ahmed Body in Spaceclaim

  • Symmetric model using combine command
  • Removing legs and moving origin to base of Ahmed body
  • Mirror command to get full model using half model

Workshop 9 : Tetra-Prism Mesh of Ahmed Body in ICEM CFD

  • Introduction
  • Y+, First cell height, and Y+ calculator in excel
  • Discussion on hybrid wall functions by Knopp
  • Boundary layer, first cell height and Yplus on Ahmed body
  • Geometry import and creation of parts
  • Global Mesh Size and Size function
  • Setting mesh sizes on parts
  • Creating density box for local mesh refinement in wake region
  • Computing volume mesh using two methods and surface mesh smoothing
  • Generating boundary layer mesh using prisms
  • Mesh export and creating three meshes for mesh independence

Workshop 9 : Problem setup and solution in Fluent

  • Problem setup in Fluent along with reference conditions
  • Solving case in Fluent with optimum settings

Workshop 9 : Post processing of flow around Ahmed Body in Fluent

  • Post processing in Fluent - Drag and Lift coefficient and comparison
  • Displaying contour plots, vector plots and path lines
  • Different type of path-lines and their settings for better flow visualization
  • Plotting experimental velocity profile at X = -163 mm in excel
  • Exporting CFD velocity profile at -163 mm and comparing with experimental data

Workshop 9 : Post Processing of Ahmed Body in CFD Post

  • Opening two cases side by side in CFD post and computing drag coefficient
  • contour plots, vectors, path-lines for Ahmed Body
  • Velocity profile at X = -163 mm in CFD post and comparison with experiments

Workshop 10 : Hexa Meshing of Ahmed Body

  • Introduction, importing spaceclaim file and creating parts
  • Workshop and course organisation
  • Initial block association and block split around Ahmed body
  • Association of blocking to Ahmed body and creating slid block for it
  • Boundary layer thickness consideration for O-Grid around Ahmed Body
  • Blocking optimization using move vertices commands based on visual observation
  • Y+ and first cell height and quality considerations for preliminary pre-mesh
  • Mesh optimization based on quality metrics
  • General mesh optimization on different regions
  • Wake region mesh refinement and general mesh refinements on different blocks
  • Getting rid of low quality regions and mesh export
  • Creating coarse, medium and fine mesh for mesh dependency study

CFD Analysis of Full P3C Orion - Part 1 : Introduction

  • Introduction

CFD Analysis of Full P3C Orion - Part 2 : Geometry Processing in Spaceclaim

  • Geaometry cleaning in spaceclaim
  • Some extra processing on model
  • Defeaturing very small features in model
  • Creating domain, making half or symmetric model and defining named selections
  • Creating another domain for aircraft

CFD Analysis of Full P3C Orion - Part 3 : Tetra Prism Meshing in ICEMCFD

  • Geometry import and considerations for high quality meshing
  • Build topology, geometry tolerance and geometry resolution issues and solution
  • Defining size function and resolving mesh issues
  • Mesh inspection from inside and repair options
  • Creating density box for mesh refinement in wake region
  • Mesh repair and some tips & tricks to improve mesh quality
  • Creating prism mesh for boundary layer capturing on aircraft
  • Editing prism mesh to increase number of layers for better capturing flow
  • Setting up solver & boundary conditions and Mesh Export for Fluent

CFD Analysis of Full P3C Orion - Part 4 : CFD solutions and results in Fluent

  • Problem setup and preliminary solution
  • Tip and tricks to speed up solution convergence and autosave files
  • Improving Y+ values
  • Results post processing : Contours, vector and XY plots
  • Results Post processing : Drag and lift Coefficients

Concluding Remarks

  • Future learning goals

Trending Courses

Popular Courses

Popular Platforms

Learn more about the Courses

Download the Careers360 App on your Android phone

Regular exam updates, QnA, Predictors, College Applications & E-books now on your Mobile

Careers360 App
150M+ Students
30,000+ Colleges
500+ Exams
1500+ E-books