All Stories

  1. Wall-Jet Evolution During Plume-Surface Interaction Using Fluorescence Imaging
  2. Towards Simultaneous Multi-Parameter Measurements Using Burst-Mode Frequency-Scanning Planar Laser-Induced Fluorescence
  3. Velocity Measurements in the Wake of the Swept Wing Flow Test Model at the National Transonic Facility
  4. Fiber-Based Multi-Resolution Imaging and Multidimensional X-Ray Diagnostics for Ejecta Dynamics in Plume Surface Interactions
  5. Wake Velocimetry of a Sphere-Cone Model in a Mach 10 Air Freestream Using FLEET
  6. Flow Visualization for Plume Surface Interaction at Martian-Relevant Lander Environments
  7. Flow visualization of intrusive and non-intrusive configurations for lunar- and Martian-relevant plume-surface interaction
  8. Demonstration of Frequency-Scanning Burst-Mode Filtered Rayleigh Scattering for Multi-Parameter Gas-Phase Measurements
  9. Development of a fs/ps CARS system for temperature measurements in supersonic and hypersonic environments
  10. Self-Aligned Focusing Schlieren at the 0.3-M Transonic Cryogenic Tunnel and the National Transonic Facility
  11. Evaluation of a Laser-Dot Grid-Projection System for Lunar Lander Crater-Shape and Ejecta-Sheet Measurements
  12. Characterization of naturally-occurring particles in the NASA Langley 0.3-m Transonic Cryogenic Tunnel using PTV
  13. FLEET and PLIF velocimetry within a Mach 10 hypersonic air flow
  14. Review of planar laser-induced fluorescence measurements in the NASA Langley 31-Inch Mach 10 Air Tunnel
  15. Development of a Terrain Mapping/Crater Evolution Measurement using Diffractive Optical Elements
  16. On the use of liquid nitrogen droplets as flow tracers in cryogenic flow facilities at NASA Langley Research Center
  17. Seeding Mechanism for High-Pressure Nozzles
  18. Velocity measurements across an oblique shock using pulse-burst cross-correlation DGV
  19. Pulse-Burst Cross-Correlation Doppler Global Velocimetry
  20. Application of Resonant Femtosecond Tagging Velocimetry in the 0.3-Meter Transonic Cryogenic Tunnel
  21. Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train
  22. Pulse-burst cross-correlation Doppler global Velocimetry
  23. Implementation of a Pulsed-laser Measurement System in the National Transonic Facility
  24. Laser Light Sheet Flow Visualization of the Space Launch System Booster Separation Test
  25. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
  26. Femtosecond Laser Tagging in R134a with Small Quantities of Air
  27. Laser Light Sheet Flow Visualization of the Space Launch System Booster Separation Test
  28. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
  29. Pulse-burst cross-correlation Doppler global velocimetery
  30. 100-kHz rate Rayleigh Imaging for Combustion and Flow Diagnostics
  31. Characterization of supersonic flows using hybrid fs/ps CARS
  32. Development of a Premixed Combustion Capability for Dual-Mode Scramjet Experiments
  33. Unseeded Velocity Measurements Around a Transonic Airfoil Using Femtosecond Laser Tagging
  34. High-Spatial-Resolution OH PLIF Visualization in a Cavity-Stabilized Ethylene-Air Turbulent Flame
  35. Optical Diagnostic Imaging of Multi-Rocket Plume-Induced Base Flow Environments
  36. Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence
  37. Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Transonic, Cryogenic Wind Tunnel
  38. A Plenoptic Multi-Color Imaging Pyrometer
  39. FLEET Velocimetry Measurements on a Transonic Airfoil
  40. Selective Two-Photon Absorptive Resonance Femtosecond-Laser Electronic-Excitation Tagging (STARFLEET) Velocimetry in Flow and Combustion Diagnostics
  41. Femtosecond Laser Tagging Characterization of a Sweeping Jet Actuator Operating in the Compressible Regime
  42. Development of Hydroxyl Tagging Velocimetry for Low Velocity Flows
  43. Femtosecond-Laser-Based Measurements of Velocity and Density in the NASA Langley 0.3-m Transonic Cryogenic Tunnel
  44. Characterization of Ablation Product Radiation Signatures of PICA and FiberForm
  45. Image Analysis of Hydroxyl-Radical Planar Laser-Induced Fluorescence in Turbulent Supersonic Combustion
  46. Visualization of Simulated Fuel–Air Mixing in a Dual-Mode Scramjet
  47. Characterization of Candidate Materials for Remote Recession Measurements of Ablative Heat Shield Materials
  48. OH PLIF Visualization of a Premixed Ethylene-fueled Dual-Mode Scramjet Combustor
  49. Investigation of Gas Seeding for Planar Laser-Induced Fluorescence in Hypersonic Boundary Layers
  50. Nonequilibrium Supersonic Freestream Studied Using Coherent Anti-Stokes Raman Spectroscopy
  51. Precision of FLEET Velocimetry using High-Speed CMOS Camera Systems
  52. Application of FLEET Velocimetry in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel
  53. Development of a Premixed Combustion Capability for Dual-Mode Scramjet Experiments (Invited)
  54. Nitric Oxide PLIF Visualization of Simulated Fuel-Air Mixing in a Dual-Mode Scramjet (Invited)
  55. Particle Image Velocimetry Applications Using Fluorescent Dye-doped Particles
  56. Background-Oriented Schlieren for Large-Scale and High-Speed Aerodynamic Phenomena (Invited)
  57. Pressure Monitoring Using Hybrid fs/ps Rotational CARS
  58. Fluorescence Imaging of Reaction Control Jets and Backshell Aeroheating of Orion Capsule
  59. Three Component Velocity and Acceleration Measurement Using FLEET
  60. Visualization of flow separation around an atmospheric re-entry capsule at low-subsonic Mach number using Background-Oriented Schlieren (BOS)
  61. High-Speed Imaging Optical Pyrometry for Study of Boron Nitride Nanotube Generation
  62. Characterization of the NASA Langley Arc Heated Scramjet Test Facility using NO PLIF
  63. Comparing Experiment and Computation of Hypersonic Laminar Boundary Layers with Isolated Roughness
  64. Dual-pump CARS of Air in a Heated Pressure Vessel up to 55 Bar and 1300 K
  65. Development of Naphthalene PLIF for Visualizing Ablation Products from a Space Capsule Heat Shield