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XIAOLIN ZHONG
XIAOLIN ZHONG
Professor of Mechanical and Aerospace Engineeirng, UCLA
Verified email at g.ucla.edu
Title
Cited by
Cited by
Year
Assessment of high-resolution methods for numerical simulations of compressible turbulence with shock waves
E Johnsen, J Larsson, AV Bhagatwala, WH Cabot, P Moin, BJ Olson, ...
Journal of Computational Physics 229 (4), 1213-1237, 2010
4262010
Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers
X Zhong, X Wang
Annual Review of Fluid Mechanics 44, 527-561, 2012
3732012
High-order finite-difference schemes for numerical simulation of hypersonic boundary-layer transition
X Zhong
Journal of Computational Physics 144 (2), 662-709, 1998
3551998
Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
Y Ma, X Zhong
Journal of Fluid Mechanics 488, 31-78, 2003
2712003
Additive semi-implicit Runge–Kutta methods for computing high-speed nonequilibrium reactive flows
X Zhong
Journal of Computational Physics 128 (1), 19-31, 1996
2711996
Stabilization of the Burnett equations and application to hypersonicflows
X Zhong, RW MacCormack, DR Chapman
AIAA journal 31 (6), 1036-1043, 1993
2181993
Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound
Y Ma, X Zhong
Journal of Fluid Mechanics 488, 79-121, 2003
2042003
Bubble dispenser in microfluidic devices
T Cubaud, M Tatineni, X Zhong, CM Ho
Physical Review E 72 (3), 037302, 2005
1972005
Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances
Y Ma, X Zhong
Journal of Fluid Mechanics 532, 63-109, 2005
1632005
Very high-order compact finite difference schemes on non-uniform grids for incompressible Navier–Stokes equations
RK Shukla, M Tatineni, X Zhong
Journal of Computational Physics 224 (2), 1064-1094, 2007
1432007
Derivation of high-order compact finite difference schemes for non-uniform grid using polynomial interpolation
RK Shukla, X Zhong
Journal of Computational Physics 204 (2), 404-429, 2005
1402005
Leading-edge receptivity to free-stream disturbance waves for hypersonic flow over a parabola
X Zhong
Journal of Fluid Mechanics 441, 315-367, 2001
1242001
A numerical study of compressible turbulent boundary layers
M Lagha, J Kim, JD Eldredge, X Zhong
Physics of fluids 23 (1), 2011
1202011
Boundary-layer receptivity of Mach 7.99 flow over a blunt cone to free-stream acoustic waves
X Zhong, Y Ma
Journal of Fluid Mechanics 556, 55-103, 2006
1182006
Numerical simulation of roughness effect on the stability of a hypersonic boundary layer
KD Fong, X Wang, X Zhong
Computers & Fluids 96, 350-367, 2014
1162014
A new high-order immersed interface method for solving elliptic equations with imbedded interface of discontinuity
X Zhong
Journal of Computational Physics 225 (1), 1066-1099, 2007
872007
A high-order cut-cell method for numerical simulation of hypersonic boundary-layer instability with surface roughness
L Duan, X Wang, X Zhong
Journal of computational physics 229 (19), 7207-7237, 2010
842010
Second mode suppression in hypersonic boundary layer by roughness: Design and experiments
KD Fong, X Wang, Y Huang, X Zhong, GR McKiernan, RA Fisher, ...
AIAA Journal 53 (10), 3138-3144, 2015
782015
Real-gas and surface-ablation effects on hypersonic boundary-layer instability over a blunt cone
CH Mortensen, X Zhong
AIAA Journal 54 (3), 980-998, 2016
752016
Linear stability analysis of nose bluntness effects on hypersonic boundary layer transition
J Lei, X Zhong
Journal of Spacecraft and Rockets 49 (1), 24-37, 2012
742012
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