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

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Bibliographic Details
Corporate Authors: AIAA/ASME Joint Thermophysics and Heat Transfer Conference Chicago, Ill.), American Institute of Aeronautics and Astronautics., American Society of Mechanical Engineers.
Format: 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

Cover

Table of contents

LEADER 11766cam a2200469 i 4500
001 kn-ocn902686213
003 OCoLC
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006 m o d
007 cr cn|||||||||
008 150203s2010 vaua ob 100 0 eng d
040 |a CUS  |b eng  |e rda  |e pn  |c CUS  |d OCLCO  |d OCL  |d OCLCO  |d OCLCA  |d OCLCQ  |d DKU  |d OCLCO  |d OCLCQ 
020 |a 9781624101397  |q (ebook) 
020 |a 1624101399  |q (ebook) 
035 |a (OCoLC)902686213 
111 2 |a AIAA/ASME Joint Thermophysics and Heat Transfer Conference  |n (10th :  |d 2010 :  |c Chicago, Ill.) 
245 1 0 |a 10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. 
246 3 |a Tenth AIAA/ASME Joint Thermophysics and Heat Transfer Conference 
246 1 |i At head of title:  |a Fluid Dynamics and co-located conferences 
264 1 |a [Reston, VA] :  |b [American Institute of Aeronautics and Astronautics],  |c [2010] 
300 |a 1 online resource (various pagings) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
500 |a A collection of technical papers from a conference held at Chicago, Illinois, 28 June-1 July 2010. 
504 |a Includes bibliographical references. 
505 8 0 |t Development of a Tool to Recreate the Mars Science Laboratory Aerothermal Environment --  |t An RSM/EVM Flow/Heat Transfer Model Applied to Pre-Transitional and Turbulent Boundary Layers --  |t Numerical Analysis of Heated Channel Flows by a Space-Marching Finite-Volume Technique --  |t Efficient Radiative Transfer Equation Solver Using the Discontinuous Galerkin Method and the GPU --  |t Heat Transfer LES Simulations in Application to Wire-Wrapped Fuel Pins --  |t Heat Conduction inside of an Irregularly Shaped Non-Convex Body Immersed in a Turbulent Hypersonic Flow Field --  |t Effect of Axial Heat Conduction and Internal Heat Generation on the Effectiveness of Counter Flow Microchannel Heat Exchangers --  |t Modeling a Phase Change Thermal Storage Device --  |t Heat Transfer Past Multiple Tube Banks: A Numerical Investigation --  |t Numerical Investigation of Jet-Obstructions to Aid in Enhancing Surface Heat Transfer from an Impinging 2D Hot-Air Jet --  |t Performance Evaluation of Atrium Smoke Exhaust System by Two Fire Models --  |t Quantification of Uncertainty in Aerodynamic Heating of a Reentry Vehicle due to Uncertain Wall and Freestream Conditions --  |t Analysis of Instabilities in Non-Axisymmetric Hypersonic Boundary Layers over Cones --  |t Computational Analysis of Arc-Jet Wedge Tests Including Ablation and Shape Change --  |t Validation of a Three-Dimensional Ablation and Thermal Response Simulation Code --  |t ExoMars Capsule Aerodynamics Analysis --  |t Three-Dimensional Aerodynamics Study for Mars Aeroshell in Nonequilibrium Flow --  |t Contribution of Vacuum-Ultraviolet (VUV) Transitions of Molecular Nitrogen to Radiation during Atmospheric Reentry --  |t Interactions of Single-Nozzle Sonic Propusive Deceleration Jets on Mars Entry Aeroshells --  |t Assessment of Turbulent CFD agaisnt STS-128 Hypersonic Flight Data 
505 8 0 |t A Unified Numerical Approach for Aerothermal-Man-Machine-Environmental System --  |t Assessment of Reaction-Rate Predictions of a Collision-Energy Approach for Chemical Reactions in Atmospheric Flows --  |t Spray Cooling Droplet Impingement Model --  |t Distributed Direct Simulation Monte Carlo Methods --  |t A Smoothed Accept-Reject Algorithm for COllissional Modeling in DSMC --  |t Particle-in-Cell Method for Solving the Boltzmann Equation --  |t DSMC Study of an H2/O2 Detonation Wave Structure --  |t Verification of an Electron-Carbon Interaction Model fro DSMC Schemes --  |t Modeling Hierarchical Thermal Transport in Electric Systems --  |t Micro Channel heat Sink with Embedded Pin-Fin Structures --  |t Characteristic Study on the Optimization of Micro Pin-Fin Heat Sink with Staggered Arrangement --  |t Development of Supersonic Retro-Propoulsion for Future Mars Entry, Descent, and Landing Systems --  |t An Initial Assessment of Navier-Stokes Codes Applied to Supersonic Retro-Propulsion --  |t Comparison of Iviscid and Viscous Aerodynamic Predictions of Supersonic Retropropulsion Flowfields --  |t Development of Thermal Protection Materials for Future Mars Entry, Descent and Landing Systems --  |t Validation Testing of a New Dual Heat Pulse, Dual Layer Thermal Protection System Applicable to Human Mars Entry, Descent and Landing --  |t Direct Coupling of the NEQAIR Radiation and DPLR CFD Codes --  |t Co-Optimization of Mid Lift to Drag Vehicle Concepts for Mars Atmsopheric Entry --  |t Comparison of Heat Transfer Measurement Devices in Arc Jet Flows with Shear --  |t Simulation of Gas-Surfacec Interactions Using ReaxFF Reactive Molecular Dynamics : Oxygen Adsorption on Platinum 
505 8 0 |t Modeling Air-SiO2 Surface Catalysis under Hypersonic Conditions with ReaxFF Molecular Dynamics --  |t Development of a Catalytic Coating for a Shuttle Flight Experiment --  |t Development of a 30 kW Inductively Coupled Plasma Torch Facility for Aerospace Material Testing --  |t Monte Carol Simulation of Atomic Oxygen Undercutting on Polymer Film --  |t Modeling Distribution of Atomic Oxygen Flux and Fluence on Spacecraft Surface in LEO Space Environment --  |t Absolute Radiation Measurement in Venus and Mars Entry Conditions --  |t Analysis of Air Radiation Measurements Obtained in the EAST and X2 Shock Tube Facilities --  |t Ablative Mateiral Testing at VKI Plasmatron Facility --  |t A Study on Ablation Behavior of Spherical Ice Piece in Hypersonic Flow --  |t Experimental and Numerical Studies of Hypersonic Flows in Rarefied Wind Tunnel --  |t Thermal Performance of a Wire Mesh/Hollow Glass Sphere Composite Structure --  |t Stagnating Radiator Thermal Model Design and Verification --  |t Experimental Study of the Natural Convection of the Wall of Infrared Balloon --  |t Local Heat Transfer Measurements inside a Compact Heat Exchanger --  |t Design of Embedded Temperature-Sensor Heat Flux Gauges for Bodies with Initial Linear Temperature Gradients --  |t Volumetric Heat Flux Characterization Experiments in the Interaction Heating Facility at NASA Ames --  |t Test Flow Conditions for the Expansion Tube Experiment --  |t Evaluation of Prediction Accuracy of Thermal Response of Ablator under Arcjet Flow Conditions --  |t Experimental and Numerical Investigation of an Unsteady Conjugate Heat Transfer Case --  |t Experimental Determination of the Key Heat Transfer Mechanisms in Pharmaceutical Freeze Drying 
505 8 0 |t Pyrolysis Mechanism of PICA --  |t Assessment of Carbon-Phenolic-in-Air Chemistry Models for Atmospheric Re-Entry --  |t Post-Test Sample Analysis of Fiber Reinforced Plastic Using Arcjet --  |t Parametric Studies with an Arc Electrode Mass Loss Model --  |t Experimental Study of Natural Frost Formation on a Horizontal Cylinder --  |t Computations of Heat Transfer in Transitional Turbine Flows --  |t Improved Temperature Extrapolation Methods for Power Plant Systems --  |t Modeling of Rocket Combustion Devices --  |t Terahertz Rayleigh Scattering of Particles in Rocket Exhaust Plumes --  |t Parallel Flow Microchannel Heat Exchangers Subjected to Axial Heat Conduction and Internal Heat Generation --  |t Porous Media Combustion for Heating Process --  |t Chemically Reacting and Particle-Laden Multiphase Flow in a Molten Salt Vessel --  |t Modeling and Simulation of Heat Transfer on Functionally Graded Materials for Hot Structures in Scramjet Engines --  |t A USM Two-Phase Subgrid Scale Stress Model for Swirling Gas-Particle Flows --  |t Knudsen Force Modeling in Application to Microsystems --  |t Experimental Study of Droplet Motion and Thermocapillary Heat Transfer in a Closed Microchannel --  |t Dynamics of Fluid Flow in a Heated Zig-Zag Square Microchannel --  |t DPD Simulation of Electroosmotic Flow in Nanochannels and the Evaluation of Effective Parameters --  |t Assessing the Potential for Condensation in Supersonic MicroNozzle Flows --  |t Development of a MEMS Based Integrated Hot-Film Flow Sensor 
505 8 0 |t Importance Sampling Based Direct Simulation Monte Carlo Method --  |t Determining the Thermal Conductivity of W/B4C Multilayer Structures Using Photothermal Deflection Spectroscopy --  |t Numerical Analysis of Convection Heat Transfer over Multiple Vaulted Roof Buildings --  |t Ice Slurry Theraml Energy Storage System --  |t Numerical Simulation of Hypersonic Blunt Body and Nozzle FLows Using Master Equation --  |t A Multi-Group Maximum Entropy MOdel for Thermo-Chemical Nonequilibrium --  |t On the Kinetic Formulation of Vibrationally Coupled Diatomic Dissociation and Montaomic Recombination --  |t VIbrational State to State Kinetics in Expanding and Compressing Nitrogen Flows --  |t Rovibrational Internal Energy Excitation and Dissociation of Molecular Nitrogen in Hypersonic Flows --  |t Energy Transfer Kinetics of Vibrationally Excited Molecules --  |t Nonequilibrium Flow Characterization in a Mach 5 Wind Tunnel --  |t Analysis of Multi-Vane Radiometers in High Altitude Propulsion --  |t Vibrational and Rotational Excitation and Dissociation in N2-N2 Collisions from Accurate Theoretical Calculations --  |t Improvement and Extension of the Loosely Coupled Navier-Stokes Code SINA to Different Gases --  |t Nonequilibrium Chemistry and Radiation for Neptune Entry --  |t Coupled Radiation-Gasdynamic Model for STARDUST Aerothermodynamic Data --  |t EMission Spectroscopic Measurements in the Plenum of the NASA IHF Arc Jet Facility --  |t Study of Radiation in Electric Arc Shock Tubes --  |t Details of Modeling Titan Entry Nonequilibrium Radiation with a Multi-Quantum Vibration State CR Model --  |t Spectral Emissivity of Shock Waves in Martian and Titan Atmospheres 
505 8 0 |t Experimental Investigation of Radiating Flux behind Strong Shock Waves in CH4:N2 Mixtures --  |t Mesh Tailoring for Strongly Coupled Computation of Ablative Material in Nonequilibrium Hypersonic Flow --  |t Modeling Gun Bore Heat Transfer & Degradation --  |t Thermal Model Correlations : Benefits, Limitations, and Best Practices --  |t The Effect of End Conditions on Laminar and Turbulent Natural Convective Flow in a High Aspect Ratio Enclosure --  |t Convective and Radiative Heat FLux Estimation on a Re-Entry Capsule --  |t Effect of Velocity-Ratio on the Mixing of Non-Isothermal Counter-Flowing Jets in a Channel --  |t Flow and Heat Transfer Characteristics Downstream of a Porous Sudden Expansion --  |t Radiation Heat-Transfer Model for the Ablation Zone of Low-Density Carbon-Resin Composites --  |t Assessing Calorimeter Evaluation Methods in Convective and Radiative Heat Flux Environment --  |t Uncertainty and Local Sensitivity Analysis of View Factors for Steady-State Conjugate Heat Transfer Problems --  |t Combined Heat Transfer in High-Porosity High-Temperature Fibrous Insulations: Theory and Experimental Validation --  |t Development of a High-Temperature Optical Coating for Thermal Management on Solar Probe Plus --  |t Atomistic Modeling of the Decomposition of Charring Ablators --  |t Ablation, Thermal Response, and Chemistry Program for Analysis of Thermal Protection Systems --  |t Multidimensional Testing of Thermal Protection Materials in the Arcjet Test Facility --  |t Radiation Testing of PICA at the Solar Power Tower. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Heat  |x Transmission  |v Congresses. 
650 0 |a Space vehicles  |v Congresses. 
650 0 |a Thermodynamics  |v Congresses. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
710 2 |a American Institute of Aeronautics and Astronautics. 
710 2 |a American Society of Mechanical Engineers. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpAIAAAS65/10th-aiaa-asme?kpromoter=marc  |y Full text 

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