Related references
Note: Only part of the references are listed.Design and optimization of aerospike nozzle for rotating detonation engine
Xiang-Yang Liu et al.
AEROSPACE SCIENCE AND TECHNOLOGY (2022)
Experimental investigation of micro-ramp control for shock train under various incoming flow conditions
Ziao Wang et al.
PHYSICAL REVIEW FLUIDS (2022)
Design of a Mach 2 shape transition nozzle for lab-scale direct-connect supersonic combustor
Bu-Kyeng Sung et al.
AEROSPACE SCIENCE AND TECHNOLOGY (2021)
Pilot hydrogen enhanced combustion in an ethylene-fueled scramjet combustor at Mach 4
Ye Tian et al.
PHYSICS OF FLUIDS (2021)
Flow response hysteresis of throat regulation process of a two-dimensional mixed-compression supersonic inlet
Yi JIN et al.
Chinese Journal of Aeronautics (2021)
Effect of pilot hydrogen on the formation of dynamic flame in an ethylene-fueled scramjet with a cavity
Wen Shi et al.
PHYSICS OF FLUIDS (2021)
Behavior and flow mechanism of shock train self-excited oscillation influenced by background waves
Wenxin Hou et al.
ACTA ASTRONAUTICA (2020)
Experimental investigation of unstart dynamics driven by subsonic spillage in a hypersonic scramjet intake at Mach 6
Manoj Kumar K. Devaraj et al.
PHYSICS OF FLUIDS (2020)
Experimental study on the forced oscillation of shock train in an isolator with background waves
Wenxin Hou et al.
AEROSPACE SCIENCE AND TECHNOLOGY (2020)
Propagation of shock-wave/boundary-layer interaction unsteadiness in attached and separated flows
Ziao Wang et al.
AIP ADVANCES (2020)
Shock train behavior affected by continuous Mach number variation of incoming flow
Wenxin Hou et al.
ACTA ASTRONAUTICA (2020)
On the unsteady throttling dynamics and scaling analysis in a typical hypersonic inlet-isolator flow
K. Raja Sekar et al.
PHYSICS OF FLUIDS (2020)
Experimental study and analysis of shock train self-excited oscillation in an isolator with background waves
Wen-xin Hou et al.
JOURNAL OF ZHEJIANG UNIVERSITY-SCIENCE A (2020)
Behavior of Shock Train in Curved Isolators with Complex Background Waves
He-xia Huang et al.
AIAA JOURNAL (2018)
Analysis of shock unsteadiness in a supersonic over-expanded planar nozzle
Shashi Verma et al.
EUROPEAN JOURNAL OF MECHANICS B-FLUIDS (2018)
Experimental investigation of mechanism and limits for shock train rapid forward movement
Kejing Xu et al.
EXPERIMENTAL THERMAL AND FLUID SCIENCE (2018)
Oscillation of the shock train in an isolator with incident shocks
Nan Li et al.
PHYSICS OF FLUIDS (2018)
Research progress on strut-equipped supersonic combustors for scramjet application
Juntao Chang et al.
PROGRESS IN AEROSPACE SCIENCES (2018)
Mathematical Model of Shock-Train Path with Complex Background Waves
Nan Li et al.
JOURNAL OF PROPULSION AND POWER (2017)
Prediction dynamic model of shock train with complex background waves
Nan Li et al.
PHYSICS OF FLUIDS (2017)
Recent research progress on unstart mechanism, detection and control of hypersonic inlet
Juntao Chang et al.
PROGRESS IN AEROSPACE SCIENCES (2017)
Unthrottled Flows with Complex Background Waves in Curved Isolators
He-xia Huang et al.
AIAA JOURNAL (2017)
Effects of dynamic backpressure on shock train motions in straight isolator
Jianhua Cai et al.
ACTA ASTRONAUTICA (2017)
Numerical Investigation of Shock-Train Response to Inflow Boundary-Layer Variations
Romain Fievet et al.
AIAA JOURNAL (2017)
Hysteresis phenomenon of hypersonic inlet at high Mach number
Xiaoliang Jiao et al.
ACTA ASTRONAUTICA (2016)
Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement
Kejing Xu et al.
AIAA JOURNAL (2016)
Pseudo-shock waves and their interactions in high-speed intakes
F. Gnani et al.
PROGRESS IN AEROSPACE SCIENCES (2016)
Accumulation of errors in numerical simulations of chemically reacting gas dynamics
N. N. Smirnov et al.
ACTA ASTRONAUTICA (2015)
Unstart Margin Characterization Method of Scramjet Considering Isolator-Combustor Interactions
Bin Qin et al.
AIAA JOURNAL (2015)
Numerical study of oblique shock-wave/boundary-layer interaction considering sidewall effects
Bo Wang et al.
JOURNAL OF FLUID MECHANICS (2015)
Experimental Investigation of Hysteresis Phenomenon for Scramjet Engine
Juntao Chang et al.
AIAA JOURNAL (2014)
Hydrogen fuel rocket engines simulation using LOGOS code
N. N. Smirnov et al.
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2014)
Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves
H. J. Tan et al.
EXPERIMENTS IN FLUIDS (2012)
A new approach for the design of hypersonic scramjet inlets
N. Om Prakash Raj et al.
PHYSICS OF FLUIDS (2012)
Velocimetry Measurements of Unstart in an Inlet-Isolator Model in Mach 5 Flow
J. L. Wagner et al.
AIAA JOURNAL (2010)
Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow
J. L. Wagner et al.
AIAA JOURNAL (2009)
Share Paper
