All Stories

  1. Measurements of an axisymmetric hypersonic shear-layer instability on a cone-cylinder-flare in quiet flow
  2. Instability and transition onset downstream of a laminar separation bubble at Mach 6
  3. Optical-Axis Spatial Sensitivity of a Simulated Focused Laser Differential Interferometer
  4. Design of an Internal Osculating Waverider Intake
  5. Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition
  6. Local Wall Cooling Effects on Hypersonic Boundary-Layer Stability
  7. Quantitative focused laser differential interferometry with hypersonic turbulent boundary layers
  8. Characterization of instability mechanisms on sharp and blunt slender cones at Mach 6
  9. Effect of surface cooling on second-mode dominated hypersonic boundary layer transition
  10. HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot
  11. Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet Tunnel
  12. Focused Laser Differential Interferometry with Contoured Tunnel Windows
  13. Separation Bubble Variation Due to Small Angles of Attack for an Axisymmetric Model at Mach 6
  14. Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 6
  15. 100 kHz PLEET velocimetry in a Mach-6 Ludwieg tube
  16. Instability Measurements on an Axisymmetric Separation Bubble at Mach 6
  17. High-Speed Schlieren Visualization of Mach 6 Flow Past a Cone with Varied Parameters
  18. Focused Laser Differential Interferometry for Hypersonic Flow Instability Measurements with Contoured Tunnel Windows
  19. 100-kHz PLEET for hypersonic flow velocity measurements in a Mach 6 Ludwieg Tube
  20. Experimental Investigation of Optical Distortion in Hypersonic Flows at Mach 6
  21. Hypersonic shock-wave/boundary-layer interactions on a cone/flare
  22. Boundary layer transition on blunt cones at hypersonic speeds
  23. HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot
  24. Visualizations of Boundary-Layer Transition on a Sharp Cone at Mach 6
  25. Visualizations of Hypersonic Boundary-Layer Transition on a Variable Bluntness Cone
  26. Effect of CO2 Concentration in the Hypersonic Boundary Layer on Second Mode Disturbances
  27. First and Fifth Hypersonic International Flight Research Experimentation’s Flight and Ground Tests
  28. Nose-Tip Bluntness Effects on Transition at Hypersonic Speeds
  29. Effects of Attitude on HIFiRE-5b Boundary-Layer Transition
  30. Disturbance Speed Measurements in a Circular Jet via Double Focused Laser Differential Interferometry
  31. Nonmodal Growth of Traveling Waves on Blunt Cones at Hypersonic Speeds
  32. Effect of Carbon-based Ablation Products on Boundary Layer Stability
  33. HIFIRE-5b Heat Flux and Boundary-Layer Transition
  34. HIFiRE-5b Flow Computations and Attitude Determination via Comparison with Flight Data
  35. Experimental Investigation of Image Distortion in a Mach 6 Hypersonic Flow
  36. Turbulent Hypersonic Flow Effects on Optical Sensor Performance
  37. Hypersonic Shock-Wave/Boundary-Layer Interactions on a Cone/Flare Model
  38. HIFiRE-5b Boundary-Layer Transition --- With Attitude
  39. Transition on a Variable Bluntness 7-Degree Cone at High Reynolds Number
  40. Nosetip bluntness effects on transition at hypersonic speeds: experimental and numerical analysis under NATO STO AVT-240
  41. HIFiRE-1 and -5 Flight and Ground Tests
  42. Correlation of HIFiRE-5a Flight Data with Computed Pressure and Heat Transfer
  43. HIFiRE-5b Heat Flux and Boundary-Layer Transition
  44. Correlation of HIFiRE-5b Flight Data With Computed Pressure and Heat Transfer for Attitude Determination
  45. Turbulent spots in hypervelocity flow
  46. Transient Startup Simulations for a Large Mach 6 Quiet Ludwieg Tube
  47. AFRL Ludwieg Tube Initial Performance
  48. Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy
  49. Boundary-Layer Stability Analysis for Stetson’s Mach 6 Blunt-Cone Experiments
  50. Disturbance and Phase Speed Measurements for Shock Tubes and Hypersonic Boundary-Layer Instability
  51. Laminar to turbulent transition on blunt cones
  52. HIFiRE-5 Boundary Layer Transition and HIFiRE-1 Shock Boundary Layer Interaction
  53. Correlation of HIFiRE-5 Flight Data With Computed Pressure and Heat Transfer
  54. Effects of Shock-Tube Cleanliness on Slender-Body Hypersonic Instability and Transition Studies at High-Enthalpy
  55. Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures
  56. Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures
  57. Turbulent Spot Observations within a Hypervelocity Boundary Layer on a 5-degree Half-Angle Cone
  58. Bubbles emerging from a submerged granular bed
  59. Carbon Dioxide Injection for Hypervelocity Boundary Layer Stability
  60. On the impact of injection schemes on transition in hypersonic boundary layers
  61. The Effect of a Porous Thrust Surface on Detonation Tube Impulse