Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Tarnavskii, G. A.
2005.
Shock-wave modes of flow at the inlet to the diffuser of a hypersonic scramjet engine: The effect of flight altitude and velocity.
High Temperature,
Vol. 43,
Issue. 1,
p.
58.
Tarnavskii, G. A.
2005.
Shock-wave modes of flow at the inlet to the diffuser of a hypersonic scramjet engine: the effect of flight altitude and velocity.
High Temperature,
Vol. 43,
Issue. 1,
p.
58.
Tarnavskii, G. A.
2005.
Shock-wave modes of flow at the inlet to the diffuser of a hypersonic scramjet engine: the effect of flight altitude and velocity.
High Temperature,
Vol. 43,
Issue. 1,
p.
58.
REN, YU-XIN
TAN, LIAN-HUA
GAO, BO
and
WU, ZI-NIU
2005.
ON THE CHARACTERISTICS OF THE MACH STEM.
Modern Physics Letters B,
Vol. 19,
Issue. 28n29,
p.
1511.
Tarnavskii, G. A.
2006.
Shock-wave flow regimes at entry into the diffuser of a hypersonic ramjet engine: Influence of physical properties of the gas medium.
Journal of Engineering Physics and Thermophysics,
Vol. 79,
Issue. 4,
p.
699.
Skews, Beric W.
2008.
Generation and visualisation of some complex shock wave interactions.
Experiments in Fluids,
Vol. 44,
Issue. 3,
p.
381.
Goldsworthy, M. J.
and
Pullin, D. I.
2009.
Mean free path effects in the shock-implosion problem.
Physics of Fluids,
Vol. 21,
Issue. 2,
de Cacqueray, Nicolas
Bogey, Christophe
and
Bailly, Christophe
2010.
Direct Noise Computation of a Shocked and Heated Jet at a Mach Number of 3.30.
de Cacqueray, Nicolas
Bogey, Christophe
and
Bailly, Christophe
2011.
Investigation of a High-Mach-Number Overexpanded Jet Using Large-Eddy Simulation.
AIAA Journal,
Vol. 49,
Issue. 10,
p.
2171.
Li, Yongzhou
Zhang, Kun Yuan
and
Nan, Xiangjun
2012.
Design of hypersonic inward turning inlets with controllable Mach number distribution.
Paton, R. T.
Skews, B. W.
Rubidge, S.
and
Snow, J.
2013.
Imploding conical shock waves.
Shock Waves,
Vol. 23,
Issue. 4,
p.
317.
Edgington-Mitchell, Daniel
Honnery, Damon R.
and
Soria, Julio
2014.
The underexpanded jet Mach disk and its associated shear layer.
Physics of Fluids,
Vol. 26,
Issue. 9,
Mölder, S.
2017.
Reflection of curved shock waves.
Shock Waves,
Vol. 27,
Issue. 5,
p.
699.
Shoev, G.
and
Ogawa, H.
2019.
Numerical study of viscous effects on centreline shock reflection in axisymmetric flow.
Physics of Fluids,
Vol. 31,
Issue. 2,
van Aswegen, Dean
Paton, Randall T.
Versluis, Michel
and
Stride, Eleanor
2019.
Curved jetting anomaly following conical shock wave reflection.
p.
10.
Wang, Jonathan
and
Freund, Jonathan
2020.
Suppression, Enhancement, and Reversal of Hydrodynamic Ejections by Dual-pulse Laser-induced Breakdowns.
Wang, Jonathan M.
and
Freund, Jonathan B.
2020.
Hydrodynamic Ejections by Dual-Pulse Laser-Induced Breakdowns.
AIAA Journal,
Vol. 58,
Issue. 8,
p.
3544.
Ren, Yu-xin
Tan, Lianhua
and
Wu, Zi-niu
2020.
The shape of incident shock wave in steady axisymmetric conical Mach reflection.
Advances in Aerodynamics,
Vol. 2,
Issue. 1,
Zhang, Enlai
Li, Zhufei
Ji, Junze
Si, Dongxian
and
Yang, Jiming
2021.
Converging near-elliptic shock waves.
Journal of Fluid Mechanics,
Vol. 909,
Issue. ,
Tashiro, Tenta
Fukunaga, Ryota
Utsunomiya, Daisuke
Nakao, Shinichiro
Miyazato, Yoshiaki
and
Ishino, Yojiro
2023.
Flow features of underexpanded microjets emerging from a round convergent nozzle.
Experiments in Fluids,
Vol. 64,
Issue. 3,