Shock train behavior affected by continuous Mach number variation of incoming flow

Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows

(2020) Wei Huang et al.   ACTA ASTRONAUTICA

A survey on numerical simulations of drag and heat reduction mechanism in supersonic/hypersonic flows

(2019) Xiwan SUN et al.   Chinese Journal of Aeronautics

Numerical investigation on the forced oscillation of shock train in hypersonic inlet with translating cowl

(2019) Wen Shi et al.   AEROSPACE SCIENCE AND TECHNOLOGY

Onset of detonation in hydrogen-air mixtures due to shock wave reflection inside a combustion chamber

(2018) N.N. Smirnov et al.   ACTA ASTRONAUTICA

Effect of back-pressure forcing on shock train structures in rectangular channels

(2018) F. Gnani et al.   ACTA ASTRONAUTICA

Control of pseudo-shock oscillation in scramjet inlet-isolator using periodical excitation

(2018) Wei-Yi Su et al.   ACTA ASTRONAUTICA

Behavior of Shock Train in Curved Isolators with Complex Background Waves

(2018) He-xia Huang et al.   AIAA JOURNAL

Nonequilibrium processes in meta-stable media⋆

(2018) N. N. Smirnov et al.   EUROPEAN PHYSICAL JOURNAL E

Experimental investigation of mechanism and limits for shock train rapid forward movement

(2018) Kejing Xu et al.   EXPERIMENTAL THERMAL AND FLUID SCIENCE

Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows

(2018) Min Ou et al.   INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER

Analysis and modelling of unsteady shock train motions

(2018) Bing Xiong et al.   JOURNAL OF FLUID MECHANICS

Investigations on flowfield behavior and resistance backpressure characteristics of supersonic cascade with boundary layer suction

(2018) Ziao Wang et al.   ACTA ASTRONAUTICA

Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl

(2018) Wen Shi et al.   ACTA ASTRONAUTICA

Oscillation of the shock train in an isolator with incident shocks

(2018) Nan Li et al.   PHYSICS OF FLUIDS

Response of Shock Train to High-Frequency Fluctuating Backpressure in an Isolator

(2017) Bing Xiong et al.   JOURNAL OF PROPULSION AND POWER

Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor

(2016) Ming-bo Sun et al.   ACTA ASTRONAUTICA

Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement

(2016) Kejing Xu et al.   AIAA JOURNAL

Shock Train/Boundary-Layer Interaction in Rectangular Isolators

(2016) Jonathan S. Geerts et al.   AIAA JOURNAL

Flow Mechanism in a Hypersonic Sidewall Compression Inlet with a Rectangular-to-Circular Isolator

(2016) Xiong Liu et al.   JOURNAL OF SPACECRAFT AND ROCKETS

Pseudo-shock waves and their interactions in high-speed intakes

(2016) F. Gnani et al.   PROGRESS IN AEROSPACE SCIENCES

Mixing augmentation induced by the interaction between the oblique shock wave and a sonic hydrogen jet in supersonic flows

(2015) Wei Huang et al.   ACTA ASTRONAUTICA

Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity

(2015) Hongbo Wang et al.   ACTA ASTRONAUTICA

Accumulation of errors in numerical simulations of chemically reacting gas dynamics

(2015) N.N. Smirnov et al.   ACTA ASTRONAUTICA

Characterization of Two Typical Unthrottled Flows in Hypersonic Inlet/Isolator Models

(2015) He-xia Huang et al.   JOURNAL OF AIRCRAFT

Hydrogen fuel rocket engines simulation using LOGOS code

(2014) N.N. Smirnov et al.   INTERNATIONAL JOURNAL OF HYDROGEN ENERGY

Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition

(2012) Ming Bo Sun et al.   EXPERIMENTAL THERMAL AND FLUID SCIENCE

Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves

(2012) H. J. Tan et al.   EXPERIMENTS IN FLUIDS

Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator

(2011) Wei Huang et al.   ACTA ASTRONAUTICA

Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows

(2011) Wei Huang et al.   ACTA ASTRONAUTICA

Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

(2009) J. L. Wagner et al.   AIAA JOURNAL