The Physics of Fluids · 1966 · 180 citations · 3 references
Natural SciencesPhysicsAerodynamicsFluid DynamicsFluid MechanicsHypersonic AerodynamicsInviscid FlowFree Jet AnalysisHypersonic FlowHypersonic Flow RegimesKinetic TheoryKnudsen NumberMach NumberMoment EquationsSource Flow
A systematic approximation has been constructed for the moment equations of kinetic theory which describe source flow expansion. For small source Knudsen number, the moments are expanded and solutions are obtained near the source. These solutions are nonuniformly valid far from the source, breaking down when transition flow is encountered. To analyze the rarefied regime, the equations are rescaled taking account that the flow is hypersonic in the transition regime. This allows us to apply a hypersonic approximation to the moment equations in the rarefied regime and subsequently match this to the inviscid solution. For spherical expansion we resolve the problem to a relaxation process with two translation temperatures, one along streamlines T∥, and the other transverse to streamlines T⊥. We obtain expressions for the terminal Mach number in terms of source Knudsen number and intermolecular force law, and a simple rarefaction criteria is found which states that transition flow is encountered when T∥ − T⊥ ≅ Tisentropic.
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Velocity Distributions in Molecular Beams from Nozzle Sources
James B. Anderson, John B. Fenn · The Physics of Fluids · 1965 · 457 citations
Engineering, Physics, Aerodynamics +12
Atomic recombination in a hypersonic wind-tunnel nozzle
K.N.C. Bray · Journal of Fluid Mechanics · 1959 · 182 citations