Ablation Analyses of Optimized Nose Tips for Hypersonic Vehicles
Ablative Materials' Boundary Condition Simulation by Applying Inverse Approach and Euler Solver
Absolute Measurements of Air Shock-Layer Radiation in the T6 Aluminium Shock Tube
This paper presents the first experimental measurements of shock-layer radiation from a new high-enthalpy ground-test facility: the T6
...Advanced Models for Vibrational and Chemical Kinetics Applied to Mars Entry Aerothermodynamics
The paper presents a comparative study of vibrational-chemical kinetics and heat transfer in carbon dioxide flows under Mars entry
...Analysis of Chemical Nonequilibrium and Elemental Demixing in Plasmatron Facility
Analysis of Segmented Arc-Heater Flows with High Argon Concentration
Analysis of Shock Deceleration Effects in the NASA Electric Arc Shock Tube
Complex processes related to nonequilibrium thermochemistry and radiation are a fundamental aspect of atmospheric entry flowfields
...Analysis of the JAXA Nonequilibrium Infrared Emission Spectra for Mars Entry Conditions
Nonequilibrium infrared emission spectra representative of a Mars atmospheric entry mission are modeled using RADIS, a spectral code for
...Application of Reflected Shock Wave Configuration to Validate Nonequilibrium Models of Reacting Air
Aspect Ratio Effects on the Noncracking and Cracking Heat Transfer in Microchannels
In cooling microchannels of advanced flight engines, the fuel temperature rapidly increases to facilitate endothermic cracking reactions
...Assessment of Classical Impulsive Models of Dissociation in Thermochemical Nonequilibrium
In strong shock waves in rarefied gases, chemical processes such as dissociation and exchange reactions occur in conditions of
...Boundary-Layer Thermochemical Analysis During Passive and Active Oxidation of Silicon Carbide
The current design of NASA’s Multi-Purpose Crew vehicle uses the latest iteration of AVCOAT, an ablating thermal protection material
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Carbon Nanotube Arrays for Enhanced Thermal Interfaces to Thermoelectric Modules
Characterization of Carbon Ablation Models Including Effects of Gas-Phase Chemical Kinetics
The modeling of the oxidation and sublimation of carbon-based ablative thermal protection system materials remains an area of active
...Characterizing High-Energy-Density Propellants for Space Propulsion Applications
Chemical Kinetic and Radiative Simulations for Titan Atmospheric Entry
Chemical-Kinetic Parameters of Hyperbolic Earth Entry
Chemical Rate Constants in Nonequilibrium Flows