All Stories

  1. Aeroheating Testing of the Mars Sample Return Earth Entry System With Surface Roughness
  2. An Approach for Practical Grid-Resolved Roughness Aerothermodynamic Simulations for Woven Heatshield Surfaces
  3. Including Radiative Heating for the Design of the Orion Backshell for Artemis-1: A Narrative
  4. Mars Sample Return Earth Entry System Woven Roughness Mach 6 Aeroheating Test
  5. Coupled Simulations of Shoulder Ablation of a Conceptual Aeroshell
  6. Efficient Two-Way Coupled Analysis of Steady-State Particle-Laden Hypersonic Flows
  7. Hayabusa2 SHARC Spectro-Radiometric Calibration and Analysis
  8. Comparison between Hayabusa 2 Spectral Measurements and Simulations
  9. Impact of Thermoelectric-Driven Flowfield Voltages on Thermocouples for Ablating Reentry Vehicles
  10. Analysis of Huygens Entry Observation to Inform Titan Shock-Layer Radiation Models
  11. Efficient Solution of Surface Erosion in Particle-Laden Hypersonic Flows
  12. Evaluating Shock-Tube Informed Biases for Shock-Layer Radiative Heating Simulations
  13. Investigation of Galileo Probe Entry Heating with Coupled Radiation and Ablation
  14. Recent Improvements to the LAURA and HARA Codes
  15. Radiative Heating on the After-Body of Martian Entry Vehicles
  16. Investigation of Galileo Probe Entry Heating with Coupled Radiation and Ablation
  17. Simulation of the Schiaparelli Entry and Comparison to Aerothermal Flight Data
  18. Evaluating Shock-Tube Informed Biases for Shock-Layer Radiative Heating Simulations
  19. Features of Afterbody Radiative Heating for Titan Entry
  20. Novel Approach for Modeling CO2 Non-equilibrium Radiation: Application to Wake Flows
  21. Impact of Non-Tangent-Slab Radiative Transport on Flowfield–Radiation Coupling
  22. Extension of Multiband Opacity-Binning to Molecular, Non-Boltzmann Shock Layer Radiation
  23. Development of a Radiative Heating Margin Policy for Lunar Return Missions
  24. Influence of Coupled Radiation and Ablation on Meteor Entries
  25. Backshell Radiative Heating on Human-Scale Mars Entry Vehicles
  26. Experimental and Numerical Investigation of Air Radiation in Superorbital Expanding Flow
  27. On the development of a new nonequilibrium chemistry model for Mars entry
  28. Impact of Non-Tangent-Slab Radiative Transport on Flowfield-Radiation Coupling
  29. Development of a Radiative Heating Margin Policy for Lunar Return Missions
  30. Novel Approach for CO2 State-To-State Modeling and Application to Multidimensional Entry Flows
  31. Equilibrium Radiative Heating from 9.5 to 15.5  km/s for Earth Atmospheric Entry
  32. Uncertainty and Sensitivity Analysis of Afterbody Radiative Heating Predictions for Earth Entry
  33. Improved Non-Boltzmann Modeling for Nitrogen Atoms
  34. A Reduced Order Maximum Entropy Model for Chemical and Thermal Non-equilibrium in High Temperature CO2 Gas
  35. Refinements to Afterbody Radiative Heating Simulations for Earth Entry
  36. Non-equilibrium Radiation for Earth Entry
  37. Uncertainty Analysis of Radiative Heating Predictions for Titan Entry
  38. Uncertainty and Sensitivity Analysis of Afterbody Radiative Heating Predictions for Earth Entry
  39. Modeling of Non-equilibrium Radiation for CO2-N2Gas Mixtures
  40. Aerothermodynamic Characteristics of 16-22 km/s Earth Entry
  41. Radiative Heating on the After-Body of Martian Entry Vehicles
  42. Uncertainty Analysis and Validation of Radiation Measurements for Earth Reentry
  43. State-to-State Modeling of CO for Mars Entry Applications
  44. Features of Afterbody Radiative Heating for Earth Entry
  45. Influence of Radiative Absorption on Non-Boltzmann Modeling for Mars Entry
  46. Mars Science Laboratory Heat Shield Aerothermodynamics: Design and Reconstruction
  47. Characterization of Stagnation-Point Heat Flux for Earth Entry
  48. Features of Afterbody Radiative Heating for Earth Entry