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Applied Mathematics and Mechanics (English Edition), ISSN 0253-4827, 02/2019, Volume 40, Issue 2, pp. 193 - 214
Journal Article
Applied Mathematics and Mechanics (English Edition), ISSN 0253-4827, 02/2019, Volume 40, Issue 2, pp. 273 - 282
Flow structures of a Mach 6 transitional boundary layer over a 260 mm long flared cone are investigated by the particle image velocimetry (PIV). Particle... 
particle image velocimetry (PIV) | direct numerical simulation (DNS) | O357.4 | hypersonic transition | O354.4 | MATHEMATICS, APPLIED | O357 | O354 | 4(+)3 | TAYLOR-GREEN | TRANSITION | 76K05 | ZIGZAG | MECHANICS | EVOLUTION | IMAGE-PREPROCESSING METHOD | VORTEX-SURFACE FIELDS | Usage | Computer-generated environments | Computer simulation | Analysis | Boundary layer
Journal Article
Applied Mathematics and Mechanics (English Edition), ISSN 0253-4827, 02/2019, Volume 40, Issue 2, pp. 283 - 292
An artificial disturbance is introduced into the boundary layer over a flat plate to investigate the effect on the transition process in the Mach 6.5 wind... 
hypersonic | glowing discharge | boundary layer | transition control | O354.4 | 76K05 | MATHEMATICS, APPLIED | MECHANICS | IMAGE-PREPROCESSING METHOD | STABILITY | O354 | Hypersonic wind tunnels | Analysis | Boundary layer | Glow discharges
Journal Article
Applied Mathematics and Mechanics (English Edition), ISSN 0253-4827, 02/2019, Volume 40, Issue 2, pp. 249 - 260
Glow discharge is introduced as an artificial disturbance to investigate the evolution of first- and second-mode instabilities in a hypersonic flat plate... 
particle image velocimetry (PIV) | hypersonic | O357.4 | glow discharge | MATHEMATICS, APPLIED | O357 | INSTABILITY | STABILITY | 76N20 | TAYLOR-GREEN | TRANSITION | 76K05 | MECHANICS | RECEPTIVITY | IMAGE-PREPROCESSING METHOD | VORTEX-SURFACE FIELDS | Hypersonic wind tunnels | Analysis | Boundary layer | Glow discharges
Journal Article
Russian Journal of Numerical Analysis and Mathematical Modelling, ISSN 0927-6467, 02/2017, Volume 32, Issue 1, pp. 1 - 12
Evolution equations of small disturbances aimed to compute the location of a laminar–turbulent transition in boundary layers by the e -method taking into... 
laminar–turbulent transition | evolution equations of small disturbances | 76K05 | method | Compressible flows | 76J20 | 76F06 | eNmethod | laminar-turbulent transition | MATHEMATICS, APPLIED | ENGINEERING, MULTIDISCIPLINARY | e(N)-method | Turbulence | Usage | Models | Mathematical models | Evolutionary algorithms | Laminar flow | Heat transfer
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2017, Volume 38, Issue 11, pp. 1601 - 1612
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2016, Volume 37, Issue 12, pp. 1615 - 1630
Journal Article
Monte Carlo Methods and Applications, ISSN 0929-9629, 12/2016, Volume 22, Issue 4, pp. 337 - 347
The steady state of a dilute gas enclosed within a rectangular cavity, whose upper and lower sides are in relative motion, is considered in the slip and early... 
microchannel | 70-08 | 76K05 | slip and jump | DSMC | rarefied gas | 76P05 | Navier–Stokes | Couette flow | 76D05 | Navier-Stokes | Usage | Gas flow | Analysis | Navier-Stokes equations | Monte Carlo method | Slip | Boundary conditions | Mathematical models | Heat transfer | Heat flux | Microchannels
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2016, Volume 37, Issue 8, pp. 1013 - 1030
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2008, Volume 29, Issue 1, pp. 51 - 60
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2010, Volume 31, Issue 8, pp. 979 - 986
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2010, Volume 31, Issue 5, pp. 535 - 544
To investigate the effect of different disturbances in the upstream, we present numerical simulation of transition for a hypersonic boundary layer on a... 
76K05 | blunt cone | Mechanics | hypersonic | Mathematics | Mathematical Modeling and Industrial Mathematics | Applications of Mathematics | O357.41 | 76F06 | transition | O354.4 | Transition | Blunt cone | Hypersonic | MATHEMATICS, APPLIED | MECHANICS | Linear systems | Analysis | Boundary layer | Angle of attack | Hypersonic boundary layer | Mathematical analysis | Disturbances | Inlets
Journal Article
by 陈皓 and Chen, Hao and 鲍麟 and Bao, Lin
Applied Mathematics and Mechanics, ISSN 0253-4827, 2/2009, Volume 30, Issue 2, pp. 163 - 174
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2005, Volume 26, Issue 1, pp. 35 - 43
Journal Article
应用数学和力学:英文版, ISSN 0253-4827, 2004, Volume 25, Issue 1, pp. 93 - 101
Three kinds of forebody model of hypersonic vehicles were studied with numerical simulation method. It shows that the two-order compressive ramp model is the... 
可压缩性 | 超音速飞机 | 数值模拟 | 空气动力学 | Navier-Stokes方程 | compressibility | 76K05 | hypersonic vehicle | Mechanics | integration of forebody-inlet | Mathematics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | V211 | MATHEMATICS, APPLIED | MECHANICS | WAVERIDER
Journal Article
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