Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Kewley, D J
1975.
Numerical study of anharmonic diatomic relaxation rates in shock waves and nozzles.
Journal of Physics B: Atomic and Molecular Physics,
Vol. 8,
Issue. 15,
p.
2565.
Ebrahim, N.A.
and
Hornung, H.G.
1975.
High-Enthalpy Nonequilibrium Carbon Dioxide Nozzle and Wedge Flows: Experiment and Calculations.
AIAA Journal,
Vol. 13,
Issue. 7,
p.
845.
MUDFORD, N.
and
STALKER, R.
1976.
The production of pulsed nozzle flows in a shock tube.
Bernzott, C.
Oertel, H.
and
Schmidt, B.
1976.
Oxygen dissociation relaxation behind oblique shocks.
Applied physics,
Vol. 11,
Issue. 3,
p.
281.
Gai, S.L.
1992.
Free piston shock tunnels: developments and capabilities.
Progress in Aerospace Sciences,
Vol. 29,
Issue. 1,
p.
1.
Mallinson, S
Gai, S
and
Mudford, N
1995.
High enthalpy, hypersonic compression corner flow.
Mallinson, S. G.
Gai, S. L.
and
Mudford, N. R.
1996.
Upstream influence and peak heating in hypervelocity shock wave/boundary-layer interaction.
Journal of Propulsion and Power,
Vol. 12,
Issue. 5,
p.
984.
Park, Chul
1996.
Experimental evaluation of real-gas phenomena in high enthalpy impulse test facilities - A review.
Mallinson, S. G.
Gai, S. L.
and
Mudford, N. R.
1996.
High-enthalpy, hypersonic compression corner flow.
AIAA Journal,
Vol. 34,
Issue. 6,
p.
1130.
Nonaka, Satoshi
Mizuno, Hiroyasu
and
Takayama, Kazuyoshi
1999.
Ballistic range measurement of shock shapes in intermediate hypersonic regime.
Nonaka, Satoshi
Mizuno, Hiroyasu
Takayama, Kazuyoshi
and
Park, Chul
2000.
Measurement of Shock Standoff Distance for Sphere in Ballistic Range.
Journal of Thermophysics and Heat Transfer,
Vol. 14,
Issue. 2,
p.
225.
KIEFER, JOHN H.
2001.
Handbook of Shock Waves.
p.
29.
Hucho, Wolf-Heinrich
Hannemann, Klaus
Martinez Schramm, Jan
and
Williamson, Charles
2007.
Springer Handbook of Experimental Fluid Mechanics.
p.
1043.
Candler, Graham
2009.
Comparison of CFD and Theoretical Post-Shock Gradients in Hypersonic Flow.
Candler, Graham V.
2010.
Comparison of CFD and theoretical post-shock gradients in hypersonic flow.
Progress in Aerospace Sciences,
Vol. 46,
Issue. 2-3,
p.
81.
Askari, S.
Shojaeefard, M.H.
and
Goudarzi, K.
2011.
Numerical and analytical solution of compressible flow over double wedge and biconvex airfoils.
Engineering Computations,
Vol. 28,
Issue. 4,
p.
441.
Dongjun, Liao
Liu, Sen
Jian, Hexiang
Aimin, Xie
Wang, Zonghao
and
Huang, Jie
2018.
Shock Wave Interactions.
p.
123.