All Stories

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