Zongyu Wu

Prof. Dr. Zongyu Wu

orcid

Research Focus & Metrics

Academic Career Length

28Years (1999-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 December 2018 in International Journal of Multiphase Flow
Verified
Journal Article
Closed access
ZWZongyu Wu
Zongyu Wu
YHYiyong Huang
Yiyong Huang
XCXiaoqian Chen
Xiaoqian Chen
XZXiang Zhang
Xiang Zhang

15 June 1999 in Physical Review B
Verified
Journal Article
Closed access
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PDPengcheng Dai
Pengcheng Dai
ZWZongyu Wu
Zongyu Wu
TAT. Angot
T. Angot
SWS.-K. Wang
S.-K. Wang
HTH. Taub
H. Taub
SES. N. Ehrlich
S. N. Ehrlich
Synchrotron x-ray scattering has been used to investigate the structure and growth of perhaps the simplest of all films: xenon physisorbed on the Ag(111) surface. High-resolution x-ray scans of the in-plane structure and lower-resolution scans (specular and nonspecular) of the out-of-plane order were performed. The Xe films were prepared under both quasiequilibrium and kinetic growth conditions, and have fewer structural defects than those investigated previously by others on graphite substrates. Under quasiequilibrium conditions, the bulk Xe-Xe spacing is reached at monolayer completion, and the monolayer and bilayer lattice constants at coexistence are inferred equal to within 0.005 Å, consistent with theoretical calculations. The Xe/vacuum interface profile for a complete monolayer and bilayer grown at quasiequilibrium is found to be sharper than for kinetically grown films. At coverages above two layers, diffraction scans along the Xe(01l) rod for quasiequilibrated films are consistent with the presence of two domains having predominantly an ABC stacking sequence and rotated 60° with respect to each other about the surface normal. Annealing of these films alters neither the population of the two domains nor the fraction of ABA stacking faults. The thickest film grown under quasiequilibrium conditions exceeds 220 Å (resolution limited). Under kinetic growth conditions, x-ray intensity oscillations at the Xe anti-Bragg position of the specular rod are observed as a function of time, indicating nearly layer-by-layer growth. Up to four complete oscillations corresponding to a film of eight layers have been observed before the intensity is damped out; the number of oscillations is found to depend on the substrate temperature, the growth rate, and the quality of the Ag(111) substrate. The specular reflectivity from kinetically grown films at nominal coverages of three and four layers has been analyzed using a Gaussian model which gives a film thickness standard deviation of 0.5 and 1.0 layers, respectively. Diffraction scans along the Xe(01l) rod of these films indicate a larger fraction of ABA stacking faults than found for thicker films. These results demonstrate the difficulty of kinetically growing Xe films thicker than two layers which have an ideal slab geometry.

1 November 2018 in Acta Astronautica
Verified
Journal Article
Closed access
ZWZongyu Wu
Zongyu Wu
YHYiyong Huang
Yiyong Huang
XCXiaoqian Chen
Xiaoqian Chen
XZXiang Zhang
Xiang Zhang
WYWen Yao
Wen Yao

18 August 2022 in Microgravity Science and Technology
Verified
Journal Article
Closed access
PDF file
ZWZongyu Wu
Zongyu Wu
KLKai Li
Kai Li
WHwei han
wei han
GLGuangyu Li
Guangyu Li
CFChengguang Fan
Chengguang Fan
BXBingui Xu
Bingui Xu

1 July 2019 in International Journal of Multiphase Flow
Verified
Journal Article
Closed access
ZWZongyu Wu
Zongyu Wu
YHYiyong Huang
Yiyong Huang
XCXiaoqian Chen
Xiaoqian Chen
XZXiang Zhang
Xiang Zhang
WYWen Yao
Wen Yao

25 May 2020 in Applied Sciences
Verified
Journal Article
Open access
PDF file
RZRuofan Zhang
Ruofan Zhang
Yong ChenYong Chen
Yong Chen
QLqi lei
qi lei
XZXiang Zhang
Xiang Zhang
ZWZongyu Wu
Zongyu Wu
With the explosive growth of space debris, collisions among space debris and spacecrafts seem to be inevitable, which may greatly threaten the structure of on-orbit spacecrafts as well as astronauts’ safety. It is of crucial importance to locate the leak source and evaluate the corresponding damage quickly and accurately to ensure the safety of astronauts and spacecraft equipment. It is widely accepted that acoustic emission method can be used to detect on-orbit leak for space station; however, accurate prediction of vacuum leak noise in space station is difficult as jet and jet noise in vacuum environments are different from those in terrestrial environment. Therefore, this paper tries to investigate sound generations of vacuum leak jet by numerically analyzing dynamics of unsteady vacuum jet flow. Specifically, numerical simulation based on realizable k-ε model is adopted to study the aerodynamic properties and the aeroacoustic characteristics. Results show that RANS turbulent model can capture the pressure fluctuation with high computation efficiency and acceptable accuracy. Secondly, leak from 1 atm to vacuum forms a supersonic flow with Mach number ranging from 2 to 3, accompanied by obvious gradients of steady density, pressure, and temperature. However, the terrestrial leak from 2 atm to 1 atm forms subsonic jet flow with gradually varying gradients of density, pressure, and temperature. Thirdly, obvious reflections of pressure perturbations at the surface, with the mean free path of air molecule being 0.6 mm, can be found and form cavity-like acoustic resonance. Such resonant mechanism contributes to harmonic acoustic properties of the vacuum jet noises besides the broadband turbulent mixing noises.