All Stories

  1. In-Situ Nanoscale Ablation
  2. Overview of the Hypersonic Test Flight KREPE-2
  3. Pyrolysis Gas Energy Transport in Ablative Material
  4. Microscale Thermal–Structural Modeling for Carbon Fibers Subjected to a Hypersonic Boundary Layer
  5. Development of two-temperature model in unified solver
  6. Coupled Simulation of Material Response using Equilibrium and Finite-Rate Ablation Models
  7. Simulation of porous carbon preform ablation in a chemically reacting environment
  8. Analysis of arc-jet sample spallation products
  9. Utilizing a retrospective cost adaptation control (RCAC) algorithm to achieve data-driven, adaptive, real-time (DART) precision meteorological forecasts
  10. Modeling spallation of carbon materials in hypersonic flows
  11. Fully Coupled Material Response and Internal Radiative Heat Transfer for Three-Dimensional Heat Shield Modeling
  12. Numerical Investigation of Film Coefficient Approximation for Chemically Reacting Boundary-Layer Flows
  13. Novel Engineering Methodology for Decoupled Aerothermal Analysis of Hypersonic Atmospheric Entry Flows
  14. Simulation of Graphite Ablation using an Overset Near Body Solver on an Adaptive Block-Structured Cartesian Off-Body Grid
  15. Study of a Two-Dimensional Shape Change of Blunt-Body Geometries at Hypersonic Conditions Using Fully Coupled Simulation
  16. Modeling of spalled particles for arc-jet test planning
  17. Radiative conductivity estimation using direct approach for fibrous materials
  18. A Kinetic Monte Carlo based analysis of graphite oxidation with realistic defect distributions
  19. Semi-Empirical 1D Material Response Modeling Using Inverse Methods
  20. Kentucky Re-Entry Universal Payload System (KRUPS): Overview of flight test via high-altitude balloon
  21. A Data-Driven Approach For Real-Time Estimation of Material Uncertainty
  22. Stochastic mechanical modeling of MMOD impact-inspired cylindrical cavities in Duocel foam
  23. Radiative Transmission and Absorption Within the Thermal Protection System of Atmospheric Entry Spacecraft
  24. Geometric Effects on Charring Ablator: Modeling the Full-Scale Stardust Heat Shield
  25. Stochastic Modeling of Elastic Behavior of Fibrous Ablators
  26. Development of Stochastic Model for Fibrous Ablators
  27. Fluid Behavior in Stochastic Porous Structures
  28. Surface Oxidation of Carbon/Carbon Composites in Hypersonic Environments
  29. Numerical reconstruction of spalled particle trajectories in an arc-jet environment
  30. Crack Modeling in Charring Ablation Materials
  31. An Immersed Boundary Method for Hypersonic Viscous Flows
  32. Permeability Calculation of a Fibrous Thermal Insulator Using the Lattice Boltzmann Method
  33. Spallation particle size analysis resulting from arc-jet experiments
  34. Micro-Scale Thermal-Structural Modeling for Carbon Fibers
  35. Radiative transmission and absorption within the ablative heat shield of hypersonic vehicles
  36. Numerical Simulation of an Arc Jet Test Section
  37. Thermal Expansion for Charring Ablative Materials
  38. Numerical Investigation of Nonlinear Structural Responses in Ablation Problem
  39. Modeling thin layers of materials in the Kentucky Aerodynamic Thermal Solver (KATS)
  40. Semi-Empirical Method for Measuring Thermal Conductivity of Fibrous Insulation Materials
  41. Sensitivity Analysis in Material Response for Ablation Problem
  42. Modeling FiberForm Oxidation in a Flow Tube using a Universal Solver
  43. Numerical analysis of time accuracy of a primitive variable-based formulation of the conservative form of the governing equations for compressible flows
  44. Calibration and Uncertainty Quantification of VISTA Ablator Material Database Using Bayesian Inference
  45. Experimental analysis of spallation particle trajectories in an arc-jet environment
  46. Retrospective cost adaptive Reynolds-averaged Navier–Stokes k – ω model for data-driven unsteady turbulent simulations
  47. An introduction to the derivation of surface balance equations without the excruciating pain
  48. Thermomechanical Coupling for Charring Ablators
  49. Modeling Gasification of Carbon Fiber Preform in Oxygen Rich Environments
  50. Development Of An Open-Source Avcoat Material Database, VISTA
  51. Development of a Universal Solver and Its Application to Ablation Problems
  52. A data-driven adaptive Reynolds-averaged Navier-Stokes k − ω model for turbulent flow
  53. Thermodynamic properties of carbon-phenolic gas mixtures
  54. Development of a three-dimensional, unstructured material response design tool
  55. Two-way strongly coupled thermo-mechanical solver for ablation problems
  56. Experimental measurements of the permeability of fibrous carbon at high-temperature
  57. A not-so-harmless experiment in predatory open access publishing
  58. Application of A New Thermal-Mechanical Coupling Solver for Ablation
  59. Characterization of Ablation Product Radiation Signatures of PICA and FiberForm
  60. Numerical and experimental analysis of spallation phenomena
  61. Effects of Water Phase Change on the Material Response of Low-Density Carbon-Phenolic Ablators
  62. Evaluation of the anisotropic radiative conductivity of a low-density carbon fiber material from realistic microscale imaging
  63. Effect of spalled particles thermal degradation on a hypersonic flow field environment
  64. Turbulence Simulation Using Direct Gradient Adaptive k-ω Model
  65. Characterization of Candidate Materials for Remote Recession Measurements of Ablative Heat Shield Materials
  66. Kentucky Re-entry Universal Payload System
  67. Numerical Study of Spallation Phenomenon in an Arc-Jet Environment
  68. Modeling the oxidation of low-density carbon fiber material based on micro-tomography
  69. Modeling of Heat Transfer Attenuation by Ablative Gases During the Stardust Reentry
  70. Numerical Investigation of Thermal Response Using Orthotropic Charring Ablative Material
  71. Effects of Water Presence on Low Temperature Phenomenon in Porous TPS Materials
  72. Comparisons of PICA In-depth Material Performance and Ablator Response Modeling from MEDLI Arc Jet Tests
  73. Kinetic Rates for Gas-Phase Chemistry of Phenolic-Based Carbon Ablator in Atmospheric Air
  74. Three dimensional radiative heat transfer model for the evaluation of the anisotropic effective conductivity of fibrous materials
  75. Numerical Investigation of Geometric Effects of Stardust Return Capsule Heat Shield
  76. Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation
  77. Numerical study of iso-Q sample geometric effects on charring ablative materials
  78. Comparison of Transport Properties Models for Flowfield Simulations of Ablative Heat Shields
  79. Multidimensional Modeling of Pyrolysis Gas Transport Inside Charring Ablative Materials
  80. Numerical Investigation of Pyrolysis Gas Blowing Pattern and Thermal Response using Orthotropic Charring Ablative Material
  81. Numerical study of spallation phenomenon in an arc-jet environment
  82. Flow-Tube Oxidation Experiments on the Carbon Preform of a Phenolic-Impregnated Carbon Ablator
  83. Investigation of the scaling of roughness and blowing effects on turbulent channel flow
  84. Numerical and experimental study of carbon fiber oxidation
  85. Simulation of Flow-tube Oxidation on the Carbon Preform of PICA
  86. Numerical Prediction of Hypersonic Flowfields Including Effects of Electron Translational Nonequilibrium
  87. Volume averaged modeling of the oxidation of porous carbon fiber material
  88. Multi-dimensional modeling of charring ablators
  89. Flow-tube Oxidation Experiments on the Carbon Preform of PICA
  90. Modeling of chemical nonequilibrium effects in a charring ablator
  91. Investigation of Turbulent Structure Modification by Momentum Injection Into Turbulent Flow Over a Rough Surface
  92. Comparison of Models for Mixture Transport Properties for Numerical Simulations of Ablative Heat-Shields
  93. Hypersonic Flow and Radiation Analysis of the Automated Transfer Vehicle Jules Verne
  94. Multi-Dimensional Modeling of Charring Ablator
  95. High performance modeling of atmospheric re-entry vehicles
  96. Modeling of heat transfer attenuation by ablative gases during the Stardust re-entry
  97. Modeling Ablation of Charring Heat Shield Materials for Non-continuum Hypersonic Flow
  98. Effect of Applied Magnetic Field on Shock Boundary Layer Interaction
  99. Numerical modeling of the CN spectral emission of the Stardust re-entry vehicle
  100. Investigation of the Effects of Electron Translational Nonequilibrium on Numerical Predictions of Hypersonic Flow Fields
  101. CFD Implementation of a novel carbon-phenolic-in-air chemistry model for atmospheric re-entry
  102. Mesh Tailoring for Strongly Coupled Computation of Ablative Material in Nonequilibrium Hypersonic Flow
  103. Assessment of Carbon-Phenolic-in-Air Chemistry Models for Atmospheric Reentry
  104. Variant of the Thomas Algorithm for opposite-bordered tridiagonal systems of equations
  105. Non-Darcian Behavior of Pyrolysis Gas in a Thermal Protection System
  106. Simulation of Pyrolysis Gas Within a Thermal Protection System
  107. Numerical solution of axisymmetric multi-species compressible gas flow: towards improved circuit breaker simulation
  108. Transient Ablation Regime in Circuit Breakers
  109. Simulation of arc-electrode interaction using sheath modelling in SF6 circuit-breakers
  110. Simulation of Inviscid Multi-Species Plasma Flow