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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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HePHAESTUS: Heat Pipe Heterogeneous Approximation of Energy and Navier-Stokes Equations, Transience, and Non-Uniform Surface Heating [Slides]
A heat pipe is a liquid/vapor filled metal pipe capable of transporting large amounts of heat through evaporation of a liquid at one end and condensation of vapor at the other end creating a closed fluid loop. Heat pipes are widely used in the cooling of electronics and in space applications. Heat pipes are typically composed of a pipe wall, a wick material, a working fluid, and a central vapor channel. Heat is transferred into the working fluid at the “evaporator” end, through an adiabatic section, and heat is removed at the opposite end at the “condenser.” If no wick is used, gravitational acceleration can circulate the fluid due to the buoyancy of the vapor in the central core and a falling film of liquid at the pipe wall forming a “thermosyphon."
Post-Detonation Fireball Thermometry via Femtosecond-Picosecond Coherent Anti-Stokes Raman Scattering (CARS).
Abstract not provided.
Coherent anti-Stoke Raman scattering thermometry in very-high-temperature systems.
Abstract not provided.
Femtosecond Coherent Anti-Stokes Raman Spectroscopy in a Cold-Flow Hypersonic Wind Tunnel for Simultaneous Pressure and Temperature Measurements.
Abstract not provided.
Burst-mode coherent anti-Stokes Raman scattering thermometry in the Sandia free-piston shock tube.
Abstract not provided.
The Navier-Stokes Equations Do Not Describe the Smallest Scales of Turbulence.
Abstract not provided.
Gas-Phase Pressure and Temperature Measurements in a Cold-Flow Hypersonic Wind Tunnel via Femtosecond Coherent Anti-Stokes Raman Spectroscopy.
Abstract not provided.
Navier-Stokes: Tensorization of the Sod and Blow-off problems [Slides]
Abstract not provided.
Gas-Phase Pressure and Temperature Measurements in a Cold-Flow Hypersonic Wind Tunnel via Femtosecond Coherent Anti-Stokes Raman Spectroscopy
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Gas Temperature Measurements in a Hypersonic Wind Tunnel via Femtosecond Coherent Anti-Stokes Raman Spectroscopy
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A Deep Least Squares Method for the Stokes Equations
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Coherent anti-Stokes Raman scattering thermometry and concentration measurements in Plasmatron X
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Hypersonic Thermal Boundary Layer Profiles via Femtosecond Coherent Anti-Stokes Raman Spectroscopy
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A Second-Order-in-Time, Explicit Approach Addressing the Redundancy in the Low-Mach, Variable-Density Navier-Stokes Equations
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Hybrid fs/ps Coherent Anti-stokes Raman Scattering for simultaneous CO/N2 concentration characterization
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