10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference.

• Corporate Authors: AIAA/ASME Joint Thermophysics and Heat Transfer Conference Chicago, Ill., American Institute of Aeronautics and Astronautics, American Society of Mechanical Engineers
• Format: Electronic eBook
• Language: English
• Published: [Reston, VA] : [American Institute of Aeronautics and Astronautics], [2010]
• Subjects: Heat > Transmission > Congresses.; Space vehicles > Congresses.; Thermodynamics > Congresses.; elektronické knihy; electronic books
• ISBN: 9781624101397; 1624101399
• Physical Description: 1 online resource (various pagings) : illustrations

Table of Contents:

• Development of a Tool to Recreate the Mars Science Laboratory Aerothermal Environment
• An RSM/EVM Flow/Heat Transfer Model Applied to Pre-Transitional and Turbulent Boundary Layers
• Numerical Analysis of Heated Channel Flows by a Space-Marching Finite-Volume Technique
• Efficient Radiative Transfer Equation Solver Using the Discontinuous Galerkin Method and the GPU
• Heat Transfer LES Simulations in Application to Wire-Wrapped Fuel Pins
• Heat Conduction inside of an Irregularly Shaped Non-Convex Body Immersed in a Turbulent Hypersonic Flow Field
• Effect of Axial Heat Conduction and Internal Heat Generation on the Effectiveness of Counter Flow Microchannel Heat Exchangers
• Modeling a Phase Change Thermal Storage Device
• Heat Transfer Past Multiple Tube Banks: A Numerical Investigation
• Numerical Investigation of Jet-Obstructions to Aid in Enhancing Surface Heat Transfer from an Impinging 2D Hot-Air Jet
• Performance Evaluation of Atrium Smoke Exhaust System by Two Fire Models
• Quantification of Uncertainty in Aerodynamic Heating of a Reentry Vehicle due to Uncertain Wall and Freestream Conditions
• Analysis of Instabilities in Non-Axisymmetric Hypersonic Boundary Layers over Cones
• Computational Analysis of Arc-Jet Wedge Tests Including Ablation and Shape Change
• Validation of a Three-Dimensional Ablation and Thermal Response Simulation Code
• ExoMars Capsule Aerodynamics Analysis
• Three-Dimensional Aerodynamics Study for Mars Aeroshell in Nonequilibrium Flow
• Contribution of Vacuum-Ultraviolet (VUV) Transitions of Molecular Nitrogen to Radiation during Atmospheric Reentry
• Interactions of Single-Nozzle Sonic Propusive Deceleration Jets on Mars Entry Aeroshells
• Assessment of Turbulent CFD agaisnt STS-128 Hypersonic Flight Data
• A Unified Numerical Approach for Aerothermal-Man-Machine-Environmental System
• Assessment of Reaction-Rate Predictions of a Collision-Energy Approach for Chemical Reactions in Atmospheric Flows
• Spray Cooling Droplet Impingement Model
• Distributed Direct Simulation Monte Carlo Methods
• A Smoothed Accept-Reject Algorithm for COllissional Modeling in DSMC
• Particle-in-Cell Method for Solving the Boltzmann Equation
• DSMC Study of an H2/O2 Detonation Wave Structure
• Verification of an Electron-Carbon Interaction Model fro DSMC Schemes
• Modeling Hierarchical Thermal Transport in Electric Systems
• Micro Channel heat Sink with Embedded Pin-Fin Structures
• Characteristic Study on the Optimization of Micro Pin-Fin Heat Sink with Staggered Arrangement
• Development of Supersonic Retro-Propoulsion for Future Mars Entry, Descent, and Landing Systems
• An Initial Assessment of Navier-Stokes Codes Applied to Supersonic Retro-Propulsion
• Comparison of Iviscid and Viscous Aerodynamic Predictions of Supersonic Retropropulsion Flowfields
• Development of Thermal Protection Materials for Future Mars Entry, Descent and Landing Systems
• Validation Testing of a New Dual Heat Pulse, Dual Layer Thermal Protection System Applicable to Human Mars Entry, Descent and Landing
• Direct Coupling of the NEQAIR Radiation and DPLR CFD Codes
• Co-Optimization of Mid Lift to Drag Vehicle Concepts for Mars Atmsopheric Entry
• Comparison of Heat Transfer Measurement Devices in Arc Jet Flows with Shear
• Simulation of Gas-Surfacec Interactions Using ReaxFF Reactive Molecular Dynamics : Oxygen Adsorption on Platinum
• Modeling Air-SiO2 Surface Catalysis under Hypersonic Conditions with ReaxFF Molecular Dynamics
• Development of a Catalytic Coating for a Shuttle Flight Experiment
• Development of a 30 kW Inductively Coupled Plasma Torch Facility for Aerospace Material Testing
• Monte Carol Simulation of Atomic Oxygen Undercutting on Polymer Film
• Modeling Distribution of Atomic Oxygen Flux and Fluence on Spacecraft Surface in LEO Space Environment
• Absolute Radiation Measurement in Venus and Mars Entry Conditions
• Analysis of Air Radiation Measurements Obtained in the EAST and X2 Shock Tube Facilities
• Ablative Mateiral Testing at VKI Plasmatron Facility
• A Study on Ablation Behavior of Spherical Ice Piece in Hypersonic Flow
• Experimental and Numerical Studies of Hypersonic Flows in Rarefied Wind Tunnel
• Thermal Performance of a Wire Mesh/Hollow Glass Sphere Composite Structure
• Stagnating Radiator Thermal Model Design and Verification
• Experimental Study of the Natural Convection of the Wall of Infrared Balloon
• Local Heat Transfer Measurements inside a Compact Heat Exchanger
• Design of Embedded Temperature-Sensor Heat Flux Gauges for Bodies with Initial Linear Temperature Gradients
• Volumetric Heat Flux Characterization Experiments in the Interaction Heating Facility at NASA Ames
• Test Flow Conditions for the Expansion Tube Experiment
• Evaluation of Prediction Accuracy of Thermal Response of Ablator under Arcjet Flow Conditions
• Experimental and Numerical Investigation of an Unsteady Conjugate Heat Transfer Case
• Experimental Determination of the Key Heat Transfer Mechanisms in Pharmaceutical Freeze Drying
• Pyrolysis Mechanism of PICA
• Assessment of Carbon-Phenolic-in-Air Chemistry Models for Atmospheric Re-Entry
• Post-Test Sample Analysis of Fiber Reinforced Plastic Using Arcjet
• Parametric Studies with an Arc Electrode Mass Loss Model
• Experimental Study of Natural Frost Formation on a Horizontal Cylinder
• Computations of Heat Transfer in Transitional Turbine Flows
• Improved Temperature Extrapolation Methods for Power Plant Systems
• Modeling of Rocket Combustion Devices
• Terahertz Rayleigh Scattering of Particles in Rocket Exhaust Plumes
• Parallel Flow Microchannel Heat Exchangers Subjected to Axial Heat Conduction and Internal Heat Generation
• Porous Media Combustion for Heating Process
• Chemically Reacting and Particle-Laden Multiphase Flow in a Molten Salt Vessel
• Modeling and Simulation of Heat Transfer on Functionally Graded Materials for Hot Structures in Scramjet Engines
• A USM Two-Phase Subgrid Scale Stress Model for Swirling Gas-Particle Flows
• Knudsen Force Modeling in Application to Microsystems
• Experimental Study of Droplet Motion and Thermocapillary Heat Transfer in a Closed Microchannel
• Dynamics of Fluid Flow in a Heated Zig-Zag Square Microchannel
• DPD Simulation of Electroosmotic Flow in Nanochannels and the Evaluation of Effective Parameters
• Assessing the Potential for Condensation in Supersonic MicroNozzle Flows
• Development of a MEMS Based Integrated Hot-Film Flow Sensor
• Importance Sampling Based Direct Simulation Monte Carlo Method
• Determining the Thermal Conductivity of W/B4C Multilayer Structures Using Photothermal Deflection Spectroscopy
• Numerical Analysis of Convection Heat Transfer over Multiple Vaulted Roof Buildings
• Ice Slurry Theraml Energy Storage System
• Numerical Simulation of Hypersonic Blunt Body and Nozzle FLows Using Master Equation
• A Multi-Group Maximum Entropy MOdel for Thermo-Chemical Nonequilibrium
• On the Kinetic Formulation of Vibrationally Coupled Diatomic Dissociation and Montaomic Recombination
• VIbrational State to State Kinetics in Expanding and Compressing Nitrogen Flows
• Rovibrational Internal Energy Excitation and Dissociation of Molecular Nitrogen in Hypersonic Flows
• Energy Transfer Kinetics of Vibrationally Excited Molecules
• Nonequilibrium Flow Characterization in a Mach 5 Wind Tunnel
• Analysis of Multi-Vane Radiometers in High Altitude Propulsion
• Vibrational and Rotational Excitation and Dissociation in N2-N2 Collisions from Accurate Theoretical Calculations
• Improvement and Extension of the Loosely Coupled Navier-Stokes Code SINA to Different Gases
• Nonequilibrium Chemistry and Radiation for Neptune Entry
• Coupled Radiation-Gasdynamic Model for STARDUST Aerothermodynamic Data
• EMission Spectroscopic Measurements in the Plenum of the NASA IHF Arc Jet Facility
• Study of Radiation in Electric Arc Shock Tubes
• Details of Modeling Titan Entry Nonequilibrium Radiation with a Multi-Quantum Vibration State CR Model
• Spectral Emissivity of Shock Waves in Martian and Titan Atmospheres
• Experimental Investigation of Radiating Flux behind Strong Shock Waves in CH4:N2 Mixtures
• Mesh Tailoring for Strongly Coupled Computation of Ablative Material in Nonequilibrium Hypersonic Flow
• Modeling Gun Bore Heat Transfer & Degradation
• Thermal Model Correlations : Benefits, Limitations, and Best Practices
• The Effect of End Conditions on Laminar and Turbulent Natural Convective Flow in a High Aspect Ratio Enclosure
• Convective and Radiative Heat FLux Estimation on a Re-Entry Capsule
• Effect of Velocity-Ratio on the Mixing of Non-Isothermal Counter-Flowing Jets in a Channel
• Flow and Heat Transfer Characteristics Downstream of a Porous Sudden Expansion
• Radiation Heat-Transfer Model for the Ablation Zone of Low-Density Carbon-Resin Composites
• Assessing Calorimeter Evaluation Methods in Convective and Radiative Heat Flux Environment
• Uncertainty and Local Sensitivity Analysis of View Factors for Steady-State Conjugate Heat Transfer Problems
• Combined Heat Transfer in High-Porosity High-Temperature Fibrous Insulations: Theory and Experimental Validation
• Development of a High-Temperature Optical Coating for Thermal Management on Solar Probe Plus
• Atomistic Modeling of the Decomposition of Charring Ablators
• Ablation, Thermal Response, and Chemistry Program for Analysis of Thermal Protection Systems
• Multidimensional Testing of Thermal Protection Materials in the Arcjet Test Facility
• Radiation Testing of PICA at the Solar Power Tower.