Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by Crossref.
Dunham, J.
1963.
A Theory of the Cylindrical Ejector Supersonic Propelling Nozzle.
The Journal of the Royal Aeronautical Society,
Vol. 67,
Issue. 625,
p.
64.
Ahren, B.
1963.
Note on the Cylindrical Ejector Supersonic Propelling Nozzle.
The Journal of the Royal Aeronautical Society,
Vol. 67,
Issue. 634,
p.
670.
Bragg, S. L.
and
Smith, S. F.
1963.
The Speed of Sound and Mach Number Effects.
The Journal of the Royal Aeronautical Society,
Vol. 67,
Issue. 634,
p.
669.
Filleul, N. le S.
1964.
[no title].
Journal of the Royal Aeronautical Society,
Vol. 68,
Issue. 643,
p.
487.
RUBINS, P. M.
and
CUNNINGHAM, T. H. M.
1965.
Shock-induced supersonic combustion in a constant-area duct.
Journal of Spacecraft and Rockets,
Vol. 2,
Issue. 2,
p.
199.
HOGE, HAROLD J.
and
SEGARS, RONALD A.
1965.
Choked flow - A generalization of the concept and some experimental data..
AIAA Journal,
Vol. 3,
Issue. 12,
p.
2177.
FELDT, WALTER T.
and
SHULMAN, YECHIEL
1966.
More Results on Solar Influenced Libration Point Motion.
AIAA Journal,
Vol. 4,
Issue. 8,
p.
1501.
PEARSON, H.
1966.
Comment on "Choked Flow: A Generalization of the Concept and Some Experimental Data''.
AIAA Journal,
Vol. 4,
Issue. 8,
p.
1502.
NORTON, DAVID J.
1970.
Generalized one-dimensional, compound compressible nozzle flow.
Journal of Spacecraft and Rockets,
Vol. 7,
Issue. 3,
p.
338.
Slavyanov, N. N.
and
Tagirov, R. K.
1971.
Experimental study of effect of specific heat ratio on gas pressure behind an annular step.
Fluid Dynamics,
Vol. 2,
Issue. 4,
p.
101.
Puzyrev, V. M.
and
Tagirov, R. K.
1975.
Calculation of the flow in ejector nozzles.
Fluid Dynamics,
Vol. 9,
Issue. 1,
p.
85.
Kraiko, A. N.
and
Lanyuk, A. N.
1977.
Effect of nonuniformities of the total enthalpy and entropy fields on the integrated characteristics of a nozzle.
Fluid Dynamics,
Vol. 11,
Issue. 3,
p.
431.
Antonov, A. N.
1978.
Effect of dilatation and compression waves on base pressure.
Soviet Applied Mechanics,
Vol. 14,
Issue. 9,
p.
973.
Meshcheryakov, E. A.
and
Sabel'nikov, V. A.
1981.
Combustion of hydrogen in a supersonic turbulent flow in a channel with simultaneous delivery of fuel and oxidant.
Combustion, Explosion, and Shock Waves,
Vol. 17,
Issue. 2,
p.
159.
Grin', V. T.
Kraiko, A. N.
and
Miller, L. G.
1981.
Decay of a shock wave at a perforated baffle.
Journal of Applied Mechanics and Technical Physics,
Vol. 22,
Issue. 3,
p.
372.
Kovalenko, A. A.
and
Lipatov, I. I.
1991.
Investigation of transition from subcritical to supercritical regime of viscous-inviscid interaction in the wake behind a flat plate.
Journal of Applied Mechanics and Technical Physics,
Vol. 32,
Issue. 3,
p.
365.
Bogolepov, V. V.
and
Lipatov, I. I.
1991.
Structure of the disturbed boundary layer near a cold surface.
Fluid Dynamics,
Vol. 26,
Issue. 1,
p.
15.
Kovalenko, A. A.
and
Lipatov, I. I.
1992.
Hypersonic flow past a plate of finite length.
Fluid Dynamics,
Vol. 26,
Issue. 5,
p.
692.
Lipatov, I
1995.
Internal 'shock' formation in the laminar boundary layer due to supercritical subcritical transition.
Lipatov, I. I.
1996.
IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers.
Vol. 35,
Issue. ,
p.
369.