Aerodynamic Separation Effect on Gas and Isotope Mixtures Induced by Invasion of the Free Jet Shock Wave Structure
- 15 February 1970
- journal article
- research article
- Published by AIP Publishing in The Journal of Chemical Physics
- Vol. 52 (4) , 1795-1802
- https://doi.org/10.1063/1.1673220
Abstract
The shock wave system of the underexpanded free jet, in a region where the pressure is in the range of 10−2 up to 1 torr, is partly invaded by background molecules, these latter being pumped and carried by the supersonic flow. When a gas mixture is introduced into the nozzle chamber and outside the shock barrel, this aspiration acts very selectively on the light molecules, and a mixture enriched in lighter species is attainable by skimming the free jet. This new aerodynamic separation effect, which is applicable to isotopic mixtures, is very strong in comparison to the efficiency of an elementary gaseous diffusion membrane.Keywords
This publication has 17 references indexed in Scilit:
- Separation of gas mixture in an axisymmetric supersonic jetInternational Journal of Heat and Mass Transfer, 1968
- Diffusive separation in shock waves and freejets of nitrogen-helium mixtures.AIAA Journal, 1968
- Measurement of Shock-Wave Structure in Helium-Argon MixturesPhysics of Fluids, 1967
- Electron-Beam Studies of Skimmer Interaction in a Free JetPhysics of Fluids, 1966
- Continuum-source molecular beamsAIAA Journal, 1965
- Hydrodynamical Theory of Diffusive Separation of Mixtures in a Free JetPhysics of Fluids, 1965
- Experimental Study of the Collimation Problem in a High-Intensity Molecular BeamPhysics of Fluids, 1965
- Structure of Weak Shock Fronts in Argon-Helium MixturesPhysics of Fluids, 1961
- Separation of Gas Mixtures in a Supersonic JetThe Journal of Chemical Physics, 1959
- On the Structure of Jets from Highly Underexpanded Nozzles Into Still AirJournal of the Aerospace Sciences, 1959