Mass spectrometric sampling in shock-tube studies.
Mass spectrometric sampling of shock tube species, studying reactions of gas components and ions diffusing through thermal layer from high temperature and pressure to low pressure
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Mass spectrometric sampling of shock tube species, studying reactions of gas components and ions diffusing through thermal layer from high temperature and pressure to low pressure
Computer program for calculating chemical equilibrium properties in shock tubes
Design, calibration, and use of radiometers to measure spectral emission in ballistic range and shock tube experiments
Widths measurements of van der Waals broadened Si I spectral lines by shock tube and scanning Fabry-Perot interferometer, using argon as perturbing gas
High enthalpy shock tube and nozzle gas flows for incident shock Mach numbers analyzed for laminar boundary layers and boundary layer transitions
Shock tube thermochemistry tables for high temperature gases
Shock tube flow analysis with dimensionless velocity number
Shock tube tabulated computer equilibrium thermodynamic properties for carbon dioxide and nitrogen mixture
Shock tube facility with high explosive driver for reentry flow conditions simulation of manned planetary flights
The principles, theoretical flow equations, calculation techniques, limitations and practical performance characteristics of basic and high performance shock tubes and shock tunnels are presented. Selected operating curves are included.
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Explore the source record for details and available documents.
Explore the source record for details and available documents.
We focus on coarse graining simulations based on the primary conservation equations, effectively codesigned physics and algorithms, and low-Mach-number corrected (LMC) hydrodynamics. Simulation methods involve LANL’s x-Radiation-Adaptive-Grid-Eulerian Large-Eddy Simulation, Besnard-Harlow-Rauenzahn (BHR) Reynolds-Averaged Navier-Stokes (RANS) approach, and Dynamic BHR – a paradigm bridging RANS and LES. A relevant question addressed relates to whether 3D RANS and RANS/LES hybrids – the industry standards for aerospace and automotive research, are presently relevant for practical variable-density applications involving shocked and accelerated interface instabilities. Furthermore, recent simulations of the GaTECH inclined mixing-layer shock-tube and NIF ICF-capsule experiments are used to demonstrate issues, challenges, and potential for 3D coarse grained LMC simulation strategies for robustly simulating complex transitional and coupled hydrodynamics-multiphysics with coarser resolution. Present LES readiness to provide accurate predictions at scale is demonstrated – whereas 3D RANS and RANS/LES bridging do not appear impactful in this context.
Thermal radiation from shock layer for lunar- return reentry vehicle simulated in shock-tube- driven hypersonic wind tunnel
Shock-tube studies of the supersonic nozzle expansion of diatomic gases, to analyze vibrational and dissociative nonequilibrium
Two thin blades are incorporated into a valve which, when closed, form a sealed compartment in the shock-tube portion of a pipeline. When forced open by an actuator, gas flows through the system.