[PDF][PDF] 激波反射现象的研究进展

杨旸, 姜宗林, 胡宗民 - 力学进展, 2012 - lxjz.cstam.org.cn
激波反射现象的研究进展 Page 1 第42 卷第2 期 力学进展 Vol. 42 No. 2 2012 年3 月25 日
ADVANCES IN MECHANICS Mar. 25, 2012 激波反射现象的研究进展 ∗ 杨旸姜宗林† 胡宗民 …

Validation of vibration-dissociation coupling models in hypersonic non-equilibrium separated flows

G Shoev, G Oblapenko, O Kunova, M Mekhonoshina… - Acta Astronautica, 2018 - Elsevier
The validation of recently developed models of vibration-dissociation coupling is discussed
in application to numerical solutions of the Navier–Stokes equations in a two-temperature …

On the transition between regular and irregular shock patterns of shock-wave/boundary-layer interactions

J Matheis, S Hickel - Journal of Fluid Mechanics, 2015 - cambridge.org
The reflection of strong oblique shock waves at turbulent boundary layers is studied
numerically and analytically. A particular emphasis is put on the transition between regular …

Dynamics study of shock wave intersection under high-frequency sine oscillation incoming flow

L Su, F Wen, Z Li, C Wan, J Han, S Wang, Z Wang - Physics of Fluids, 2022 - pubs.aip.org
This paper numerically studies the dynamics of symmetrical wedge shock intersection under
sinusoidal supersonic oscillation conditions. The 15 symmetrical wedges are used as the …

Mach stem height and growth rate predictions

CA Mouton, HG Hornung - AIAA journal, 2007 - arc.aiaa.org
CONSIDER the reflection of a shock, generated by a wedge in steady supersonic flow, from
a wall (single wedge configuration) or from a plane of symmetry (double wedge …

Reflection and transition of planar curved shock waves

T Zhang, K Xu, C Shi, C Zhu, Y You - Journal of Fluid Mechanics, 2023 - cambridge.org
In this paper, the reflection of curved shock waves over a symmetry plane in planar
supersonic flow is studied. This includes stable Mach reflection (MR) and the regular …

Dynamics of unsteady asymmetric shock interactions

L Laguarda, S Hickel, FFJ Schrijer… - Journal of Fluid …, 2020 - cambridge.org
The response of asymmetric and planar shock interactions to a continuous excitation of the
lower incident shock is investigated numerically. Incident shock waves and centred …

Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel

MS Ivanov, AN Kudryavtsev, SB Nikiforov… - Physics of …, 2003 - pubs.aip.org
Experiments on the transition between steady regular and Mach reflections of shock waves
have been performed in a low-noise wind tunnel. Owing to a very low level of free-stream …

Experimental investigation of shock–shock interactions with variable inflow Mach number

L Laguarda, J Santiago Patterson, FFJ Schrijer… - Shock Waves, 2021 - Springer
Experiments on shock–shock interactions were conducted in a transonic–supersonic wind
tunnel with variable free-stream Mach number functionality. Transition between the regular …

Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream

K Naidoo, BW Skews - Journal of fluid mechanics, 2011 - cambridge.org
There have been numerous studies on the steady-state transition criteria between regular
and Mach reflection of shock waves generated by a stationary, two-dimensional wedge in a …