ME 651: Fluid Dynamics Autumn 2014
Rajneesh Bhardwaj Department of Mechanical Engineering IIT Bombay
ME 651: Fluid Dynamics Autumn 2014 Rajneesh Bhardwaj Department of - - PowerPoint PPT Presentation
ME 651: Fluid Dynamics Autumn 2014 Rajneesh Bhardwaj Department of Mechanical Engineering IIT Bombay Timings and Venue Timings : SLOT 13, Mondays and Thursdays, 6:30 to 7:55 pm; Venue : CDEEP, A1A2 classroom, Mathematics building
Rajneesh Bhardwaj Department of Mechanical Engineering IIT Bombay
Timings and Venue
Instructor and TAs
Instructor:
Teaching Assistants:
Emails: atulsoti@gmail.com, hemanshul.garg@gmail.com
Grading Policy
Course outline
Streaklines, Streamlines; Kinematic decomposition of velocity field.
fluid; Rates of deformation and development of the constitutive equations of Fluid Dynamics (Stokes' relations); The Navier-Stokes (N-S) Equations; Special forms of the N-S equations; Initial and Boundary conditions; Differential form of Thermal and Mechanical energy equations; Introduction to non- dimensionalization and scaling; Non-dimensional numbers of interest in incompressible flow; Classification
Course outline
incompressible N-S equations (e.g. Couette and Poiseuille flows, Flow between rotating cylinders, Stokes' First and Second problems, Stagnation point flow, Flow over a porous wall, etc.).
theorem; Irrotationality; Simple Potential Flows; Superposition; Technique of Images; Introduction to the use of complex variables for plane Potential Flows; Introduction to lifting surfaces.
Interaction of vortices.
Course outline
analysis and development of Prandtl's boundary layer equations; Blasius' solution to flat plate; Boundary layer with pressure gradient (Falkner-Skan solutions); von-Karman-Pohlhausen integral analysis method; Boundary layer separation and control.
turbulence - role of vorticity and viscosity; Statistical description; Reynolds' averaging of N-S equations; Reynolds' stresses; Kinetic energy budget in turbulent flow; Wall turbulence: eddy diffusivity, Prandtl's mixing length hypothesis, von-Karman's stability hypothesis; Universal velocity profile.
Acoustic waves; Normal shock waves; Basic one-dimensional compressible flow in a duct with varying cross-sectional area; One-dimensional compressible flow with friction and heat transfer.
References
Mc-Graw Hill, 3rd ed, 2012
Policy towards attendance
course:
department, and warn the students about the attendance rules of the Institute (For attendance less than 80%, the student will be awarded “XX” grade )."
rare situations (medical emergency etc) will be forwarded to Dean (Acad) for
proxy attendance cases will be dealt strictly.
Policy towards cheating
– Permitting any other student (s) to copy any part of your answer sheet – Copying off someone else's answer sheet, texting on a cellphone for answers and bringing in cheat sheets in examination hall.
according to institute rules. This could also result in 'F' (fail grade) in the course.
should add ME651 in the subject line while contacting me via email. This is for filtering
used for recording lectures while entering in class late.
Flow past a circular cylinder
Wave energy converter in ocean dcml.pratt.duke.edu/fsi.shtml
Re = 100
Courtesy: Prof E Panides, Columbia University
Courtesy: Prof E Panides, Columbia University
Courtesy: Prof E Panides, Columbia University
Courtesy: Prof E Panides, Columbia University
Dimensionless time Perturbation pressure
2 4 6 8 10
2E-05 4E-05 6E-05 8E-05 0.0001 0.00012
Present work Analytical, Liu and Vasilyev (2007)
Cylinder
Acoustics source
Compressible flows
Pressure perturbation at t = 0 Probe A
Perturbation pressure at Probe A
No slip velocity BC Neumann pressure BC No slip velocity BC Neumann pressure BC Neumann velocity BC Neumann pressure BC Dirichlet velocity BC Neumann pressure BC
FSI Benchmark: Flow past an elastic plate mounted on a stationary cylinder
Deformable surface Prescribed force BC Fixed surface Probe on plate (tip)
Turek and Hron, 2006
boundary
Vorticity field Dimensionless time Ytip Xtip
20 40 60 80 1 1.5 2 2.5 3 5 5.5 6 6.5 7
Ytip Xtip
Dynamics of the elastic plate
Bhardwaj and Mittal, 2011
A bug on water surface
100 rpm 300 rpm 600 rpm
Inkjet printing Spie.org
Droplet dispensing Xiong et al 1998
Courtesy: Prof E Panides, Columbia University
High speed visualization Numerical model
Droplet impact on a solid surface
Bhardwaj, Longtin and Attinger, 2010
31
Fluid dynamics and heat transfer during non-isothermal impact
1 mm t = 0 ms 3 ms 5 ms 7 ms 10 ms 15 ms 20 ms 25 ms T: 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
Parameters: Isopropanol drop on fused silica, d0 = 1.8 mm (3 microliter), v0 = 0.37 m/s, Initial drop and substrate temperature = 23oC and 68 oC, respectively
T(oC): 23 27.5 32 36.5 41 45.5 50 54.5 59 63.5 68
T: 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 90 ms 1 mm 30 ms T: 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 60 ms 40 ms
32 Particle visualization in evaporating nanoliter water droplet on glass
50 µm
Microscope Water drop with fluorescent particles Glass slide
100 µm
t = 0 s 3.3 s 6.6 s 9.9 s
Bhardwaj, Fang and Attinger, 2009
3 s 3.3 s 3.5 s 3.8 s 100 µµ Increase in particles concentration at stagnation point Particle moves radially outward Particle returns to stagnation point 1 2 3 4
X 4 1 2 3
r z Particle visualization in evaporating nanoliter isopropanol droplet on PDMS
35
Phonation Cardic flows Nih.gov Wikipedia.org Hemodynamics of aneurysms in coronary arteries or aorta
Courtesy: X Zheng And R. Mittal JHU
Impingement of Blast Wave on Human Eye
Blast source Applications in understanding combat ocular injuries Compressible flow field outside eye Non uniform and highly transient pressure loading on cornea Shock propagation inside Newtonian and viscoelastic fluid Fluid-Structure interaction of Newtonian/viscoelastic fluid with Isotropic/Anisotropic and Elastic/hyperelastic Material Vitreous humor (Visocoelastic fluid) Aqueous humor (Newtonian fluid) Lens (Isotropic material) Cornea and Sclera (Anisotropic and hyperelastic Material)
Shock propagation
Bhardwaj et al., 2013
Bhardwaj et al., 2013
Dimensionless time Dimensionless piston velocity
20 40 60 80 100
0.2 0.4
Diastole Systole E-wave A-wave Simulation performed for this stage
Parameters
and peak mitral jet velocity)
peak mitral jet velocity and duration of E-wave)
Piston
X Y 2 4 6 8 10 12 1 2 3 4 5
Left Ventricle Left Atrium Mitral Valves Prescribed force BC (deformable surface) Hinged point Neumann BC for pressure and velocity
Upiston
Hinged point No slip Neumann BC for pressure No slip Neumann BC for pressure
Flow induced deformation of mitral leaflets in left ventricle
Pathologies of mitral leaflets are implicated in many heart conditions including mitral-valve stenosis and prolapse induced regurgitation Bhardwaj and Mittal, 2011
Velocity of the piston Acceleration of the piston t = 0.5 t = 7.0 t = 11.5 t = 17.0 t = 24.0 t = 29.0
A B C D E F
Left ventricular hemodynamics
Vorticity scale
42
Opening and closing of mitral leaflets is influenced by piston acceleration Vortex ring is formed by the rolling of the mitral jet by viscous forces of the quiescent fluid in the left ventricle Formation time of vortex ring has been correlated to heart conditions by Gharib et al., 2007