Wu,
ChinTien


Address: 
Department
of Applied Mathematics 

Phone: 
035712121ext56424 

email: 

Vitae
Research Plan
Teaching
Statement
· Existence and regularity of capillary surface over unbounded domain,
Master thesis,
· Geometrically Nonlinear Analysis of Lightweight
Composite Space Reflector using Solid Shell Elements Based on the Assume Strain
Formulation
Technical Report, GSFC 2000. (Presented in FEMCI workshop 2001 by Keejoo Lee)
·
On the implementation of an
accurate and efficient solver for the convectiondiffusion equations Ph.D.
Thesis, UMCP 2003.
·
A comparison of
geometric and algebraic multigrid for discrete convectiondiffusion equations
Presented in 8th Copper Mountain Conference on Iterative Methods 2004.
·
Analysis and comparison
of geometric and algebraic multigrid for convectiondiffusion equations
accepted by SIAM SISC 06/2006
·
Stopping criteria for iterative
methods in solving convectiondiffusion equations on adaptive meshes.
Presented in the third international congress of chinese mathematicians, 2004. To be submitted.
·
An efficient
semicoarsening multigrid method for variable diffusion problems in cylindrical
coordinates Accepted by Journal of Applied Numerical Mathematics. 02/2006.
· An efficient multigrid solver of transient 2D NavierStokes equations for incompressible flows. In preparation.
· An introduction of
multigrid method for large scale computation, Lecture note in Scientific
Computing,
· An introduction of
Maltab programming for scientific computations, Lecture note in Dept.
Applied Math. NCTU,
Calculus Class
Webpage for Students
Two snap shots from my
convectiondiffusion solver
Remaining interfaces are still under construction.
Some results from my 2D NavierStokes
Calculation:
l
KVS at Renold's number
100 KVS at
Renold's number 1000 
l Airfoil NACA0012 NACA0012 at
10 degree of angle of attack, Re=4000 NACA0012 at
34 degree of angle of attack, Re=1000 




l FluidStructure interaction Flow past an oscillating cylinder with Reynold’s number 200, oscillating frequency=0.1 and oscillating amplitude=0.4 
locally moving meshes for trancient computation 
History of changing of the drag and lift coefficients:
