All Stories

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