steady and unsteady compressible flows

  • 格式:pdf
  • 大小:1.19 MB
  • 文档页数:74

Part B: Recent In-House Efforts in Compressible Flows 1. 2. 3. 4. Heat transfer at Mach 2 Sod's Shock tube Lagrange gun validation with user-defined real gas V-22 with tiltrotors (meshing and dynamic mesh)
• •
What is the motivation for this session?
3
Motivation for this session
In their call for papers, the organizers included a special section on steady and unsteady compressible flows in order to: • Bring together various persons who use FLUENT for computing compressible flows; • Invite FLUENT users to showcase their work on compressible flows; • Communicate FLUENT’s capabilities pertaining to compressible flows; • Discuss techniques that are unique to compressible flows; • Facilitate the exchange of ideas on solving compressible flow problems.
7
Acknowledgement
A quick thanks to two of my colleagues for reviewing the contents of this presentation with me: • Dr. Thomas Scheidegger, Application Specialist for Unsteady Flows (and, less officially, Gambit guru); • Dr. Laith Zori, FLUENT developer, specialist for the coupled solvers and compressible flows (we go back all the way to grad school at Iowa State University).
Let us begin with the first presentation!
5
A Fluent Perspective on Compressible Flows
A presentation at the session “Steady and Unsteady Compressible Flows” at the 2005 UGM
8
Outline
Part A: New Developments in Compressible Flows 1. 2. 3. New numerics in FLUENT 6.2 New features in FLUENT 6.2 Beta features in FLUENT 6.3
Part B: Recent In-House Efforts in Compressible Flows 1. 2. 3. 4. Heat transfer at Mach 2 Sod's Shock tube Lagrange gun validation with user-defined real gas V-22 with tiltrotors (meshing and dynamic mesh)
11
Part A: New Developments 1. New Numerics in FLUENT 6.2
New numerics for all solvers: Third order MUSCL scheme (discretization of the convection terms):
14
Part A: New Developments 1. New Numerics in FLUENT 6.2
New numerics for all solvers: Automated Full MultiGrid (FMG) initialization: • With this method, we compute an inviscid (Euler) solution as our initial “guess”; • We compute this Euler solution using the coupled explicit solver’s FAS-multigrid capability: • • • • the FAS agglomerates cells to produce a series of meshes; We obtain an Euler solution on the coarsest mesh; We interpolate onto the next finer mesh, and solve on that mesh; Continue until we reach the original (finest) mesh;
12
Part A: New Developments 1. New Numerics in FLUENT 6.2
New numerics for all solvers: Third order MUSCL scheme (discretization of the convection terms): • A blend of central differencing and 2nd order upwinding; • It uses a combination of the cell-center values, the reconstruction gradients at the cell-centers, and the reconstructed cell-vertex (node) values; node face centroid c 1 n1 f1-2 c2 cell center
13
Part A: New Developments 1. New Numerics in FLUENT 6.2
New numerics for all solvers: Third order MUSCL scheme (discretization of the convection terms): • Expect more accurate predictions for forces/moments, vortices, and secondary flows; • May not work well if shocks are present because it does not utilize flux-limiters (one may see undershoots/overshoots); • With structured quad/hex meshes, continue to use the QUICK scheme for the convection terms;
Dr. Christoph Hiemcke, Fluent Inc.
6
Outline
Part A: New Developments in Compressible Flows 1. 2. 3. New numerics in FLUENT 6.2 New features in FLUENT 6.2 Beta features in FLUENT 6.3
What is the timetable for this session?
4
Timetable for this session
There will be four presentations:
1. First 30 minutes. Presentation by Christoph Hiemcke, Fluent, Inc. "A Fluent perspective on compressible flows". 2. Second 20 minutes: Jim DeSpirito "Evaluation of Synthetic Jets for Munition Control" 3. Third 20 minutes: Daniel Cler "The Changing Role of Fluid Mechanics and CFD in the Design of Gun Systems" 4. Fourth 20 minutes: Kent Misegades "Extraction of boundary layer characteristics from FLUENT results".
9
Part A: New Developments 1. New Numerics in FLUENT 6.2
• In FLUENT 6.2, there are a number of new numerical schemes that will help solve compressible flow problems; • These were mentioned during the product presentations, but let’s have a closer look; • We begin with new numerics that are available in both the segregated and the coupled solvers: