Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Edelman, Louis M.
and
Gamba, Mirko
2019.
Time Delay Response of a Mach 2 Pseudo-Shock to Downstream Forcing.
Lusher, David J.
and
Sandham, Neil D.
2020.
Shock-Wave/Boundary-Layer Interactions in Transitional Rectangular Duct Flows.
Flow, Turbulence and Combustion,
Vol. 105,
Issue. 2,
p.
649.
Lee, Gyu Sub
Baccarella, Damiano
Liu, Qili
Elliott, Gregory S.
and
Lee, Tonghun
2020.
Pseudoshock Dimensionality in Axisymmetric and Rectangular Scramjets.
Baccarella, Damiano
Liu, Qili
McGann, Brendan
and
Lee, Tonghun
2020.
Isolator Shock Dynamics of Mass Injection-Induced Unstart in a Circular Model Scramjet.
Edelman, Louis M.
and
Gamba, Mirko
2020.
Structure of a Mach 2 Shock Train from Experimental Measurements.
Wang, Ziao
Chang, Juntao
Hou, Wenxin
and
Yu, Daren
2020.
Propagation of shock-wave/boundary-layer interaction unsteadiness in attached and separated flows.
AIP Advances,
Vol. 10,
Issue. 10,
Baccarella, Damiano
Liu, Qili
Lee, Gyu Sub
and
Lee, Tonghun
2020.
Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5.
Hunt, Robin
and
Hunt, Gregory
2020.
Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information.
Wang, Ziao
Chang, Juntao
Wu, Guangwei
and
Yu, Daren
2021.
Experimental investigation of shock train behavior in a supersonic isolator.
Physics of Fluids,
Vol. 33,
Issue. 4,
Baccarella, D.
Liu, Q.
McGann, B.
Lee, G.
and
Lee, T.
2021.
Isolator-combustor interactions in a circular model scramjet with thermal and non-thermal choking-induced unstart.
Journal of Fluid Mechanics,
Vol. 917,
Issue. ,
Li, Nan
Chang, Juntao
Xu, Kejing
Yu, Daren
and
Bao, Wen
2021.
Instability of shock train behaviour with incident shocks.
Journal of Fluid Mechanics,
Vol. 907,
Issue. ,
Edelman, Louis M.
Gamba, Mirko
Hunt, Robin
Auslender, Aaron
Donbar, Jeffrey M.
and
Hagenmaier, Mark
2021.
Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock.
Chin, Jared
and
Gamba, Mirko
2021.
Machine learning applications for shock train diagnostics.
Leonard, Michael D.
and
Narayanaswamy, V.
2021.
Investigation of shock dynamics in an axisymmetric inlet/isolator with attached boundary layers.
Journal of Fluid Mechanics,
Vol. 908,
Issue. ,
Wang, Ziao
Chang, Juntao
Kong, Chen
and
Li, Yunfei
2021.
Micro-Ramp Control for Shock Train Structure and Oscillation.
AIAA Journal,
Vol. 59,
Issue. 12,
p.
4881.
Petha Sethuraman, Vignesh Ram
Kim, Tae Ho
and
Kim, Heuy Dong
2021.
Effects of back pressure perturbation on shock train oscillations in a rectangular duct.
Acta Astronautica,
Vol. 179,
Issue. ,
p.
525.
Huang, Tinglong
Zhang, Qifan
Yue, Lianjie
Zhang, Peng
and
Zhao, Qingjun
2021.
Hysteresis of Shock Train Movement in the Isolator with a Ramp.
AIAA Journal,
Vol. 59,
Issue. 10,
p.
3873.
Yi, Wang
Bing, Xiong
and
Xiaoqiang, Fan
2021.
Forced oscillation phenomenon of normal/oblique shock trains in a rectangular duct at Mach 2 and 3.
Acta Astronautica,
Vol. 182,
Issue. ,
p.
110.
Petha Sethuraman, Vignesh Ram
Kim, Tae Ho
and
Kim, Heuy Dong
2021.
Control of the oscillations of shock train using boundary layer suction.
Aerospace Science and Technology,
Vol. 118,
Issue. ,
p.
107012.
Xu, Shangcheng
Wang, Yi
Wang, Zhenguo
Fan, Xiaoqiang
and
Xiong, Bing
2022.
Experimental investigations of hypersonic inlet unstart/restart process and hysteresis phenomenon caused by angle of attack.
Aerospace Science and Technology,
Vol. 126,
Issue. ,
p.
107621.