2003
DOI: 10.13182/fst03-a359
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Experimental Investigation of a Shock-Accelerated Liquid Layer with Imaging and Pressure Measurement

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Cited by 3 publications
(2 citation statements)
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“…In Z-pinch IFE there are essentially three configurations of protection that need to be addressed: a conical top plug containing flibe shields the top, flowing liquid layers protecting the side walls, and a two-phase (bubbling) pool at the bottom of the chamber. Studies concerning the flowing liquid layers in shock tube experiments verified that several layers separated with a void significantly reduce the wall loading [32], and there may exist an optimum void-space-toliquid-thickness ratio to minimize the impulse force and reduce the liquid sheet break-up. Work is ongoing to study and model the shock attenuation and energy absorption in solid foam layers and in two-phase pools for the upper and lower protection schemes proposed in Z-pinch reactor designs.…”
Section: High Average Power Laser and Z-pinch Programsmentioning
confidence: 99%
“…In Z-pinch IFE there are essentially three configurations of protection that need to be addressed: a conical top plug containing flibe shields the top, flowing liquid layers protecting the side walls, and a two-phase (bubbling) pool at the bottom of the chamber. Studies concerning the flowing liquid layers in shock tube experiments verified that several layers separated with a void significantly reduce the wall loading [32], and there may exist an optimum void-space-toliquid-thickness ratio to minimize the impulse force and reduce the liquid sheet break-up. Work is ongoing to study and model the shock attenuation and energy absorption in solid foam layers and in two-phase pools for the upper and lower protection schemes proposed in Z-pinch reactor designs.…”
Section: High Average Power Laser and Z-pinch Programsmentioning
confidence: 99%
“…so as to have parallel walls to perform flow visualization anywhere along the tube~e.g., Ref. 60!. The facility's structural capability allows for the production of Mach-5 shock waves in air at atmospheric pressure.…”
Section: Ivb5 Uw Shock Tube Facilitymentioning
confidence: 99%