1 Simulation of Compressible Flow around the Bullet Trains Project Members: Tatiya SameeyaiB5212828 Cheerawan Thetchanda B5228591 Project Advisor: Assist.Prof.Dr.Keerati.

Slides:



Advertisements
Similar presentations
Outline Overview of Pipe Flow CFD Process ANSYS Workbench
Advertisements

A Computational Framework for Simulating Flow around Hypersonic Re-Entry Vehicles David Stroh, Anthony Marshik and Gautham Krishnamoorthy, UND Chemical.
University of Western Ontario
SIEMENS, MUELHEIM 1 1 Fluid-Structure Interaction for Combustion Systems Artur Pozarlik Jim Kok FLUISTCOM SIEMENS, MUELHEIM, 14 JUNE 2006.
The Flame Deflector and Five Segment Booster By: Geoffrey Husk.
Turbine-less Ducted Fan Jet Engine Subsonic Propulsion
High Performance Computing in the SCRamjet Design Project HPC User Forum Meeting Roanoke, April /21/091 Chris Larson, Axel Dietrich.
M. R. Tetlow and C.J. Doolan School on Mechanical Engineering
Airbreathing Hypersonics Laboratory China Aerodynamics Research and Development Center Osculating Inward turning Cone Waverider/Inlet (OICWI) Design Analysis.
MAE 5130: VISCOUS FLOWS Introduction to Boundary Layers
An Analysis of Hiemenz Flow E. Kaufman and E. Gutierrez-Miravete Department of Engineering and Science Rensselaer at Hartford.
Marcello Tobia Benvenuto
VISCOUS CFD ANALYSIS OF GENERIC MISSILE WITH GRID FINS By Swapnil. D
Computational Modeling of Flow over a Spillway In Vatnsfellsstífla Dam in Iceland Master’s Thesis Presentation Chalmers University of Technology 2007.
CFD and Thermal Stress Analysis of Helium-Cooled Divertor Concepts Presented by: X.R. Wang Contributors: R. Raffray and S. Malang University of California,
Pharos University ME 352 Fluid Mechanics II
Computational Fluid Dynamics (CFD) Study on the Influence of Airflow Patterns on Carbon Dioxide Distribution and Emission Rate in a Scaled Livestock Building.
Aerodynamic Study of Go-kart Nose Cones ME450 Introduction to Computer Aided Engineering Becker, Joe Professor H. U. Akay May 1, 2000.
Computer Simulations of Wind Tunnel Experiments
Team 18: Design Optimization of a Supersonic Nozzle
Experimental investigations of the flow during the stage separation of a space transportation system Andrew Hay Aerospace Engineering with German.
Engineering H191 - Drafting / CAD The Ohio State University Gateway Engineering Education Coalition Lab 4P. 1Autumn Quarter Transport Phenomena Lab 4.
Verification and Validation Diagram of a Control Rod Guide Tube on top of a hot box dome that has been gradually heating up. A hole was drilled here to.
Introduction to Fluid Mechanics
Intercollegiate Rocket Engineering Competition Spring 2015 EML Ethics and Design Project Organization.
WLTP Annex 4 and 7, delta cd*A
Wing Embedded Engines For Large Blended Wing Body Aircraft
Introduction to COMSOL Travis Campbell Developed for CHE 331 – Fall 2012 Oregon State University School of Chemical, Biological and Environmental Engineering.
A. Spentzos 1, G. Barakos 1, K. Badcock 1 P. Wernert 2, S. Schreck 3 & M. Raffel 4 1 CFD Laboratory, University of Glasgow, UK 2 Institute de Recherche.
Knowledge Extraction from Aerodynamic Design Data and its Application to 3D Turbine Blade Geometries Lars Graening
Engineering 1182 College of Engineering Engineering Education Innovation Center Solid Modeling Introduction Rev: , AJPSolid Modeling Introduction1.
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Review: Bernoulli Equation and Examples Mechanical and Aerospace Engineering Department Florida Institute of.
COSMOS FloWorks Wind Tunnel Simulation
Pharos University ME 253 Fluid Mechanics II
CFD Pre-Lab 2 Simulation of Turbulent Flow around an Airfoil Seong Mo Yeon, and Timur Dogan 11/12/2013.
Mathematical Equations of CFD
CHAPTER 1 INTRODUCTION.  At the end of this chapter, you should be able to: 1. Understand the basic concepts of fluid mechanics and recognize the various.
3 th International Symposium on Integrating CFD and Experiments in Aerodynamics U.S. Air Force Academy, CO, USA June 20-21, 2007 Integration of CFD and.
MODELLING OF MULTIPHASE FLOWS OVER SURFACE WITH PENETRABLE ROUGH RELIEF Yevgeniy A. Shkvar National Aviation University, Kyiv, Ukraine
Soliton for PDEs Math 6399 – Lec 2 Zhijun Qiao Department of Mathematics The University of Texas – Pan American Sept 2, 2008.
Computational Fluid Dynamics Applied to the Analysis of 10-mm Hydrocyclone Solids Separation Performance S. A. Grady, M. M. Abdullah, and G. D. Wesson.
ME 101: Fluids Engineering Chapter 6 ME Two Areas for Mechanical Engineers Fluid Statics –Deals with stationary objects Ships, Tanks, Dams –Common.
Fluid Mechanics SEMESTER II, 2010/2011
CFD Study of the Development of Vortices on a Ring Wing
CFD Lab 1 Simulation of Turbulent Pipe Flow Seong Mo Yeon, Timur Dogan, and Michael Conger 10/07/2015.
उद्यमेन हि सिद्ध्यन्ति
Turbulence Models Validation in a Ventilated Room by a Wall Jet Guangyu Cao Laboratory of Heating, Ventilating and Air-Conditioning,
CFD predictions of transition and distributed roughness over a wind turbine airfoil ESTEBAN FERRER XABIER MUNDUATE 47th AIAA Aerospace Sciences Meeting.
Lecture Objectives Review wall functions Discuss: Project 1, HW2, and HW3 Project topics.
05:53 Fluid Mechanics Basic Concepts.
Indian Institute of Space Science and Technology STUDY OF EFFECT OF GAS INJECTION OVER A TORPEDO ON FLOW-FIELD USING CFD.
CFD Simulation Investigation of Natural Gas Components through a Drilling Pipe RASEL A SULTAN HOUSSEMEDDINE LEULMI.
Investigation of supersonic and hypersonic laminar shock/boundary-layer interactions R.O. Bura, Y.F.Yao, G.T. Roberts and N.D. Sandham School of Engineering.
TRANSPORT OF CONTAMINANTS BY ATMOSPHERIC DUST AND AEROSOL Paola L. Colmenares Chemical Engineering University of Arizona Research supported by: NIEHS Superfund.
ANSYS. Overview of ANSYS It is an engineering simulation software developed in 1970 by Dr. John A. Swanson It was developed to use finite element analysis.
AERODYNAMIC OPTIMIZATION OF REAR AND FRONT FLAPS ON A CAR UNIVERSITY OF GENOVA – POLYTECHNIC SCHOOL ADVANCED FLUID DYNAMICS COURSE 2015/2016 Student: Giannoni.
Effects of Ventilation Systems on Ammonia Concentration Distributions in Manure-Belt Egg Layer Houses Using Computational Fluid Dynamics Xinjie Tong1.
Prepared By S.S.Pon Sudhir Sajan AP/ Aeronautical Engineering/NIU
Rotors in Complex Inflow, AVATAR, WP2
STAR Global Conference 2017
The application of an atmospheric boundary layer to evaluate truck aerodynamics in CFD “A solution for a real-world engineering problem” Ir. Niek van.
A unify analysis of isotropic and composite Belleville Spring
CONCEPT FEASIBILITY STUDY OF USING DUAL-STREAM JETS IN COLD SPRAY
Streamlining.
A unify analysis of isotropic and composite Belleville Spring
Simulation of Compressible Flow around the Bullet Trains
Investigation of Flow Turning in a Natural Blockage
Headlines here in upper and lower case
Headlines here in upper and lower case
Headlines here in upper and lower case
Presentation transcript:

1 Simulation of Compressible Flow around the Bullet Trains Project Members: Tatiya SameeyaiB Cheerawan Thetchanda B Project Advisor: Assist.Prof.Dr.Keerati Suluksna School of Aeronautical Engineering, Institute of Engineering, Suranaree University of Technology P R O J E C T Engineering EP-255X-X-XX

2 Background P R O J E C T Engineering Fig.1 The original model of bullet train head is usually encountered with shock effect during it run through the tunnel because of rapidly change in density of air between outside-to-inside zone of tunnel. Fig.2 New model of bullet train head is designed like the king fisher bird to resolve the effect of shock.

3 Objective P R O J E C T Engineering  To Simulate the aerodynamics behavior around the two model of bullet trains, original and kingfisher models, under the condition of compressible flow.

4 Scopes P R O J E C T Engineering  Two models of bullet train heads, original and king fisher model, are determined in the project activities.  Three flow speed of 250, 270, 300 km/hr have been investigated in the simulation.  The simulation will be investigated under the condition of turbulence compressible flow by means of CFD method with ANSYS Fluent 12.0  Tunnel bore size of 6.4 m will be considered here.

5 Expectation  The behaviors of air flow around the two models of bullet train head, the original and king fisher models, under the conditions of viscous and incompressible flow based on turbulence model prediction.  Comparison results of wall shear stress of two those models due to the skin friction. P R O J E C T Engineering

6 P R O J E C T Engineering Activities CAD Files Creation Fig.3 Bullet train geometries created from computer program for the original model (top) and new model (bottom)

7 Original Model: Simulation results under the condition of (upper) incompressible flow and (lower) compressible flow New Model (King fisher model): Simulation results under the condition of (upper) incompressible flow and (lower) compressible flow P R O J E C T Engineering Activities Simulation Results: Wall Shear Stress Fig.4 Comparison of predicted wall shear stress for the two considered models: (left) Original model and (right) New model (King fisher model)

8 P R O J E C T Engineering Project Plan Activities Week 1Week 2Week 3Week 4Week 5Week 6Week 7Week 8Week 9Week 10Week 11 1Survey the project information 2Practice on software and validation 3Create CAD models 4Simulate the air flow 5Conclusion and Report writing

9 THANK YOU Q & A P R O J E C T Engineering