Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Martin, F.J.
and
White, D.R.
1958.
The formation and structure of gaseous detonation waves.
Symposium (International) on Combustion,
Vol. 7,
Issue. 1,
p.
856.
Duff, Russell E.
1959.
Shock-Tube Performance at Low Initial Pressure.
The Physics of Fluids,
Vol. 2,
Issue. 2,
p.
207.
NAGAMATSU, H. T.
GEIGER, R. E.
and
SHEER, R. E.
1960.
Real Gas Effects in Flow over Blunt Bodies at Hypersonic Speeds.
Journal of the Aerospace Sciences,
Vol. 27,
Issue. 4,
p.
241.
Lin, Shao-Chi
and
Fyfe, Walter I.
1961.
Low-Density Shock Tube for Chemical Kinetics Studies.
The Physics of Fluids,
Vol. 4,
Issue. 2,
p.
238.
Russell, David A.
1962.
Orifice Plates in a Shock Tube.
The Physics of Fluids,
Vol. 5,
Issue. 4,
p.
499.
Patch, R.W.
1965.
Absolute intensity measurements for the 2·7 μ band of water vapor in a shock tube.
Journal of Quantitative Spectroscopy and Radiative Transfer,
Vol. 5,
Issue. 1,
p.
137.
Stalker, R. J.
1965.
An approximate theory of gun tunnel behaviour.
Journal of Fluid Mechanics,
Vol. 22,
Issue. 04,
p.
657.
Smith, C. Edward
1966.
The starting process in a hypersonic nozzle.
Journal of Fluid Mechanics,
Vol. 24,
Issue. 04,
p.
625.
RAKICH, JOHN V.
1967.
Three-dimensional flow calculation by the method of characteristics..
AIAA Journal,
Vol. 5,
Issue. 10,
p.
1906.
LADERMAN, A. J.
1967.
Shock-tube performance with area divergence at the diaphragm section..
AIAA Journal,
Vol. 5,
Issue. 10,
p.
1904.
Hartunian, R.A.
1968.
Atomic and Electron Physics - Atomic Interactions.
Vol. 7,
Issue. ,
p.
141.
Davies, C
and
Simpson, D
1970.
Production of hypersonic shock waves at one atmosphere.
Journal of Physics E: Scientific Instruments,
Vol. 3,
Issue. 12,
p.
1000.
PATCH, R.
1971.
SHOCK TUBE TECHNIQUE FOR MEASURING OPACITIES AT HIGH PRESSURES FOR GASEOUS-CORE NUCLEAR ROCKETS.
Dain, C G
and
Hodgson, J P
1974.
Generation of Weak Shock Waves in a Shock Tube.
Aeronautical Quarterly,
Vol. 25,
Issue. 2,
p.
101.
Gvozdeva, L. G.
and
Zhilin, Yu. V.
1978.
Experimental investigation of gasdynamic processes at sudden start-up of a supersonic nozzle.
Journal of Applied Mechanics and Technical Physics,
Vol. 18,
Issue. 4,
p.
484.
McKenna, K. F.
Bartsch, R. R.
Commisso, R. J.
Ekdahl, C.
Quinn, W. E.
and
Siemon, R. E.
1980.
Collisionless flow and end loss from a high-energy theta-pinch plasma.
The Physics of Fluids,
Vol. 23,
Issue. 7,
p.
1443.
Dongen, M. E. H. Van
Van, R. B.
Van Eck, P.
Hagebeuk, H. J. L.
Hirschberg, A.
Hutten-Mansfeld, A. C. B.
Jager, H. J.
and
Willems, J. F. H.
1981.
Influence of relaxation processes on the structure of a thermal boundary layer in partially ionized argon.
Journal of Plasma Physics,
Vol. 26,
Issue. 1,
p.
147.
Bershader, Daniel
1981.
Fluid Dynamics.
Vol. 18,
Issue. ,
p.
785.
Takano, Y
and
Akamatsu, T
1984.
A diaphragmless shock tube.
Journal of Physics E: Scientific Instruments,
Vol. 17,
Issue. 8,
p.
644.
ATKINS, H.
1988.
Numerical and analytical study of the inlet startup process in a shock tunnel environment.