All Stories

  1. Measurements of an axisymmetric hypersonic shear-layer instability on a cone-cylinder-flare in quiet flow

    Article • Physical Review Fluids, August 2023, American Physical Society (APS)

    Dr. Elizabeth Benitez, Prof. Joseph S Jewell

  2. Instability and transition onset downstream of a laminar separation bubble at Mach 6

    Article • Journal of Fluid Mechanics, August 2023, Cambridge University Press

    Dr. Elizabeth Benitez, Prof. Joseph S Jewell

  3. Design of an Internal Osculating Waverider Intake

    Article • Journal of Propulsion and Power, May 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  4. Optical-Axis Spatial Sensitivity of a Simulated Focused Laser Differential Interferometer

    Article • AIAA Journal, January 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell, Dr. Elizabeth Benitez

  5. Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition

    Article • AIAA Journal, November 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  6. Local Wall Cooling Effects on Hypersonic Boundary-Layer Stability

    Article • Journal of Spacecraft and Rockets, October 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Furkan Oz, Prof. Joseph S Jewell

  7. Quantitative focused laser differential interferometry with hypersonic turbulent boundary layers

    Article • Applied Optics, October 2022, Optical Society of America (OSA)

    Prof. Joseph S Jewell, Dr. Elizabeth Benitez

  8. Characterization of instability mechanisms on sharp and blunt slender cones at Mach 6

    Article • Journal of Fluid Mechanics, February 2022, Cambridge University Press

    Prof. Joseph S Jewell

  9. Effect of surface cooling on second-mode dominated hypersonic boundary layer transition

    Article • Experiments in Fluids, June 2021, Springer Science + Business Media

    Prof. Joseph S Jewell

  10. Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet Tunnel

    Article • AIAA Journal, January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  11. HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot

    Article • Journal of Spacecraft and Rockets, January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  12. Separation Bubble Variation Due to Small Angles of Attack for an Axisymmetric Model at Mach 6

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Elizabeth Benitez, Prof. Joseph S Jewell

  13. Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 6

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Jeffrey Komives, Prof. Joseph S Jewell, Jonathan Hill

  14. Focused Laser Differential Interferometry with Contoured Tunnel Windows

    Article • AIAA Journal, December 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Elizabeth Benitez, Prof. Joseph S Jewell

  15. 100 kHz PLEET velocimetry in a Mach-6 Ludwieg tube

    Article • Optics Express, July 2020, Optical Society of America (OSA)

    Prof. Joseph S Jewell

  16. Instability Measurements on an Axisymmetric Separation Bubble at Mach 6

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell, Dr. Elizabeth Benitez

  17. High-Speed Schlieren Visualization of Mach 6 Flow Past a Cone with Varied Parameters

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  18. Focused Laser Differential Interferometry for Hypersonic Flow Instability Measurements with Contoured Tunnel Windows

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Elizabeth Benitez, Prof. Joseph S Jewell

  19. 100-kHz PLEET for hypersonic flow velocity measurements in a Mach 6 Ludwieg Tube

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  20. Experimental Investigation of Optical Distortion in Hypersonic Flows at Mach 6

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  21. Hypersonic shock-wave/boundary-layer interactions on a cone/flare

    Article • Experimental Thermal and Fluid Science, December 2019, Elsevier

    Prof. Joseph S Jewell

  22. Boundary layer transition on blunt cones at hypersonic speeds

    Article • AIAA Journal, November 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Pedro Paredes, Meelan Choudhari, Prof. Joseph S Jewell

  23. HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  24. Visualizations of Boundary-Layer Transition on a Sharp Cone at Mach 6

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Stuart Laurence, Prof. Joseph S Jewell

  25. Visualizations of Hypersonic Boundary-Layer Transition on a Variable Bluntness Cone

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Stuart Laurence, Prof. Joseph S Jewell

  26. Effect of CO2 Concentration in the Hypersonic Boundary Layer on Second Mode Disturbances

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell, Jeffrey Komives

  27. First and Fifth Hypersonic International Flight Research Experimentation’s Flight and Ground Tests

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Karen T Berger, Prof. Joseph S Jewell

  28. Nose-Tip Bluntness Effects on Transition at Hypersonic Speeds

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Meelan Choudhari, Prof. Joseph S Jewell, Pedro Paredes

  29. Effects of Attitude on HIFiRE-5b Boundary-Layer Transition

    Article • Journal of Spacecraft and Rockets, January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  30. Disturbance Speed Measurements in a Circular Jet via Double Focused Laser Differential Interferometry

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  31. Nonmodal Growth of Traveling Waves on Blunt Cones at Hypersonic Speeds

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell, Dr. Meelan Choudhari, Pedro Paredes

  32. Effect of Carbon-based Ablation Products on Boundary Layer Stability

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell, Jeffrey Komives

  33. HIFIRE-5b Heat Flux and Boundary-Layer Transition

    Article • Journal of Spacecraft and Rockets, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  34. HIFiRE-5b Flow Computations and Attitude Determination via Comparison with Flight Data

    Article • Journal of Spacecraft and Rockets, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  35. Experimental Investigation of Image Distortion in a Mach 6 Hypersonic Flow

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  36. Turbulent Hypersonic Flow Effects on Optical Sensor Performance

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  37. Hypersonic Shock-Wave/Boundary-Layer Interactions on a Cone/Flare Model

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  38. HIFiRE-5b Boundary-Layer Transition --- With Attitude

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  39. Transition on a Variable Bluntness 7-Degree Cone at High Reynolds Number

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  40. Nosetip bluntness effects on transition at hypersonic speeds: experimental and numerical analysis under NATO STO AVT-240

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  41. HIFiRE-1 and -5 Flight and Ground Tests

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  42. Correlation of HIFiRE-5a Flight Data with Computed Pressure and Heat Transfer

    Article • Journal of Spacecraft and Rockets, September 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  43. HIFiRE-5b Heat Flux and Boundary-Layer Transition

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  44. Correlation of HIFiRE-5b Flight Data With Computed Pressure and Heat Transfer for Attitude Determination

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  45. Turbulent spots in hypervelocity flow

    Article • Experiments in Fluids, March 2017, Springer Science + Business Media

    Prof. Joseph S Jewell

  46. Transient Startup Simulations for a Large Mach 6 Quiet Ludwieg Tube

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  47. AFRL Ludwieg Tube Initial Performance

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  48. Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy

    Article • AIAA Journal, January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  49. Boundary-Layer Stability Analysis for Stetson’s Mach 6 Blunt-Cone Experiments

    Article • Journal of Spacecraft and Rockets, October 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  50. Disturbance and Phase Speed Measurements for Shock Tubes and Hypersonic Boundary-Layer Instability

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  51. Laminar to turbulent transition on blunt cones

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  52. HIFiRE-5 Boundary Layer Transition and HIFiRE-1 Shock Boundary Layer Interaction

    Article • October 2015, Defense Technical Information Center (DTIC)

    Prof. Joseph S Jewell

  53. Correlation of HIFiRE-5 Flight Data With Computed Pressure and Heat Transfer

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  54. Effects of Shock-Tube Cleanliness on Slender-Body Hypersonic Instability and Transition Studies at High-Enthalpy

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  55. Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures

    Article • January 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  56. Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures

    Article • January 2013, Defense Technical Information Center (DTIC)

    Prof. Joseph S Jewell

  57. Turbulent Spot Observations within a Hypervelocity Boundary Layer on a 5-degree Half-Angle Cone

    Article • June 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  58. Bubbles emerging from a submerged granular bed

    Article • Journal of Fluid Mechanics, January 2011, Cambridge University Press

    Prof. Joseph S Jewell

  59. Carbon Dioxide Injection for Hypervelocity Boundary Layer Stability

    Article • January 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  60. On the impact of injection schemes on transition in hypersonic boundary layers

    Article • June 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell

  61. The Effect of a Porous Thrust Surface on Detonation Tube Impulse

    Article • June 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Joseph S Jewell