All Stories

  1. Firefly Blue Ghost Mission 1: SCALPSS 1.1 Camera Calibration
  2. Firefly Blue Ghost Mission 1: SCALPSS 1.1 Long Focal Length Camera Descent Imaging
  3. Firefly Blue Ghost Mission 1: SCALPSS 1.1 Short Focal Length Camera Descent Imaging
  4. Firefly Blue Ghost Mission 1: SCALPSS 1.1 Post-Landing Terrain Measurements
  5. Firefly Blue Ghost Mission 1: SCALPSS 1.1 Payload and Mission Overview
  6. High-Speed Imaging of Atomic Oxygen Emission in the HyMETS Arcjet Tunnel
  7. Initial Measurements of Plume Impingement in the NASA Langley 60-foot Vacuum Sphere
  8. Wall-Jet Evolution During Plume-Surface Interaction Using Fluorescence Imaging
  9. Towards Simultaneous Multi-Parameter Measurements Using Burst-Mode Frequency-Scanning Planar Laser-Induced Fluorescence
  10. Velocity Measurements in the Wake of the Swept Wing Flow Test Model at the National Transonic Facility
  11. Fiber-Based Multi-Resolution Imaging and Multidimensional X-Ray Diagnostics for Ejecta Dynamics in Plume Surface Interactions
  12. Wake Velocimetry of a Sphere-Cone Model in a Mach 10 Air Freestream Using FLEET
  13. Flow Visualization for Plume Surface Interaction at Martian-Relevant Lander Environments
  14. Flow visualization of intrusive and non-intrusive configurations for lunar- and Martian-relevant plume-surface interaction
  15. Demonstration of Frequency-Scanning Burst-Mode Filtered Rayleigh Scattering for Multi-Parameter Gas-Phase Measurements
  16. Development of a fs/ps CARS system for temperature measurements in supersonic and hypersonic environments
  17. Self-Aligned Focusing Schlieren at the 0.3-M Transonic Cryogenic Tunnel and the National Transonic Facility
  18. Evaluation of a Laser-Dot Grid-Projection System for Lunar Lander Crater-Shape and Ejecta-Sheet Measurements
  19. Characterization of naturally-occurring particles in the NASA Langley 0.3-m Transonic Cryogenic Tunnel using PTV
  20. FLEET and PLIF velocimetry within a Mach 10 hypersonic air flow
  21. Review of planar laser-induced fluorescence measurements in the NASA Langley 31-Inch Mach 10 Air Tunnel
  22. Development of a Terrain Mapping/Crater Evolution Measurement using Diffractive Optical Elements
  23. On the use of liquid nitrogen droplets as flow tracers in cryogenic flow facilities at NASA Langley Research Center
  24. Seeding Mechanism for High-Pressure Nozzles
  25. Velocity measurements across an oblique shock using pulse-burst cross-correlation DGV
  26. Pulse-Burst Cross-Correlation Doppler Global Velocimetry
  27. Application of Resonant Femtosecond Tagging Velocimetry in the 0.3-Meter Transonic Cryogenic Tunnel
  28. Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train
  29. Pulse-burst cross-correlation Doppler global Velocimetry
  30. Implementation of a Pulsed-laser Measurement System in the National Transonic Facility
  31. Laser Light Sheet Flow Visualization of the Space Launch System Booster Separation Test
  32. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
  33. Femtosecond Laser Tagging in R134a with Small Quantities of Air
  34. Laser Light Sheet Flow Visualization of the Space Launch System Booster Separation Test
  35. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
  36. Pulse-burst cross-correlation Doppler global velocimetery
  37. 100-kHz rate Rayleigh Imaging for Combustion and Flow Diagnostics
  38. Characterization of supersonic flows using hybrid fs/ps CARS
  39. Development of a Premixed Combustion Capability for Dual-Mode Scramjet Experiments
  40. Unseeded Velocity Measurements Around a Transonic Airfoil Using Femtosecond Laser Tagging
  41. High-Spatial-Resolution OH PLIF Visualization in a Cavity-Stabilized Ethylene-Air Turbulent Flame
  42. Optical Diagnostic Imaging of Multi-Rocket Plume-Induced Base Flow Environments
  43. Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence
  44. Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Transonic, Cryogenic Wind Tunnel
  45. A Plenoptic Multi-Color Imaging Pyrometer
  46. FLEET Velocimetry Measurements on a Transonic Airfoil
  47. Selective Two-Photon Absorptive Resonance Femtosecond-Laser Electronic-Excitation Tagging (STARFLEET) Velocimetry in Flow and Combustion Diagnostics
  48. Femtosecond Laser Tagging Characterization of a Sweeping Jet Actuator Operating in the Compressible Regime
  49. Development of Hydroxyl Tagging Velocimetry for Low Velocity Flows
  50. Femtosecond-Laser-Based Measurements of Velocity and Density in the NASA Langley 0.3-m Transonic Cryogenic Tunnel
  51. Characterization of Ablation Product Radiation Signatures of PICA and FiberForm
  52. Image Analysis of Hydroxyl-Radical Planar Laser-Induced Fluorescence in Turbulent Supersonic Combustion
  53. Visualization of Simulated Fuel–Air Mixing in a Dual-Mode Scramjet
  54. Characterization of Candidate Materials for Remote Recession Measurements of Ablative Heat Shield Materials
  55. OH PLIF Visualization of a Premixed Ethylene-fueled Dual-Mode Scramjet Combustor
  56. Investigation of Gas Seeding for Planar Laser-Induced Fluorescence in Hypersonic Boundary Layers
  57. Nonequilibrium Supersonic Freestream Studied Using Coherent Anti-Stokes Raman Spectroscopy
  58. Precision of FLEET Velocimetry using High-Speed CMOS Camera Systems
  59. Application of FLEET Velocimetry in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel
  60. Development of a Premixed Combustion Capability for Dual-Mode Scramjet Experiments (Invited)
  61. Nitric Oxide PLIF Visualization of Simulated Fuel-Air Mixing in a Dual-Mode Scramjet (Invited)
  62. Particle Image Velocimetry Applications Using Fluorescent Dye-doped Particles
  63. Background-Oriented Schlieren for Large-Scale and High-Speed Aerodynamic Phenomena (Invited)
  64. Pressure Monitoring Using Hybrid fs/ps Rotational CARS
  65. Fluorescence Imaging of Reaction Control Jets and Backshell Aeroheating of Orion Capsule
  66. Three Component Velocity and Acceleration Measurement Using FLEET
  67. Visualization of flow separation around an atmospheric re-entry capsule at low-subsonic Mach number using Background-Oriented Schlieren (BOS)
  68. High-Speed Imaging Optical Pyrometry for Study of Boron Nitride Nanotube Generation
  69. Characterization of the NASA Langley Arc Heated Scramjet Test Facility using NO PLIF
  70. Comparing Experiment and Computation of Hypersonic Laminar Boundary Layers with Isolated Roughness
  71. Dual-pump CARS of Air in a Heated Pressure Vessel up to 55 Bar and 1300 K
  72. Development of Naphthalene PLIF for Visualizing Ablation Products from a Space Capsule Heat Shield