Shock wave driven by a phased implosion
Journal Article
·
· Physics of Fluids A; (USA)
- Theoretical Division, Los Alamos National Laboratory, Los Alamos, New Mexico 87545 (US)
- Dynamic Testing Division, Los Alamos National Laboratory, Los Alamos, New Mexico 87545 (USA)
In this paper the theory of an axially phased radial implosion of a channel is developed. When the phase velocity of the implosion exceeds the sound velocity inside the channel, a planar shock wave traveling along the channel axis can develop. For the energy of the implosion system in the appropriate range, the theory predicts a stable steady-state flow configuration. The effect of the phased implosion is for the channel wall to form a nozzle that travels along the channel axis. The flow behind the axial shock is well described by the equations for nozzle flow with an additional dynamical degree of freedom for the shape of the wall. Experiments presented here verify the theoretical predictions. The numerical simulations show the formation of the axial shock during start-up and the approach to steady state to be in good agreement with experiment and theory. A potential application of the axially phased implosion is the design of a super shock tube.
- OSTI ID:
- 6045146
- Journal Information:
- Physics of Fluids A; (USA), Journal Name: Physics of Fluids A; (USA) Vol. 3:1; ISSN 0899-8213; ISSN PFADE
- Country of Publication:
- United States
- Language:
- English
Similar Records
Generating strong shock waves with a supersonic peristaltic pump
Examination of the shock wave regular reflexion phenomenon in a rarefied supersonic plasma flow
Nonlinear interactions in superfluid dynamics: nonstationary heat transfer due to second sound shock waves. Final report
Conference
·
Mon Dec 31 23:00:00 EST 1990
·
OSTI ID:5860451
Examination of the shock wave regular reflexion phenomenon in a rarefied supersonic plasma flow
Journal Article
·
Fri Dec 31 23:00:00 EST 2004
· Physics of Plasmas
·
OSTI ID:20657966
Nonlinear interactions in superfluid dynamics: nonstationary heat transfer due to second sound shock waves. Final report
Technical Report
·
Fri Dec 31 23:00:00 EST 1982
·
OSTI ID:5836644
Related Subjects
42 ENGINEERING
420400 -- Engineering-- Heat Transfer & Fluid Flow
640410* -- Fluid Physics-- General Fluid Dynamics
75 CONDENSED MATTER PHYSICS
SUPERCONDUCTIVITY AND SUPERFLUIDITY
ALKANES
CYLINDERS
DESIGN
DETONATIONS
HEXANE
HYDROCARBONS
IMPLOSIONS
MATHEMATICS
NOZZLES
NUMERICAL ANALYSIS
ORGANIC COMPOUNDS
PHASE VELOCITY
SHOCK TUBES
SHOCK WAVES
SIMULATION
STABILITY
STEADY-STATE CONDITIONS
TUBES
USES
VELOCITY
420400 -- Engineering-- Heat Transfer & Fluid Flow
640410* -- Fluid Physics-- General Fluid Dynamics
75 CONDENSED MATTER PHYSICS
SUPERCONDUCTIVITY AND SUPERFLUIDITY
ALKANES
CYLINDERS
DESIGN
DETONATIONS
HEXANE
HYDROCARBONS
IMPLOSIONS
MATHEMATICS
NOZZLES
NUMERICAL ANALYSIS
ORGANIC COMPOUNDS
PHASE VELOCITY
SHOCK TUBES
SHOCK WAVES
SIMULATION
STABILITY
STEADY-STATE CONDITIONS
TUBES
USES
VELOCITY