All Stories

  1. Computations for a Subsonic Wind Tunnel and Discrepancies In As-Built vs. As-Designed CFD Simulations
  2. Summary of Data from the VT-NASA Blind Validation CFD Challenge Case
  3. Experimental Results for the VT-NASA CFD Turbulence Model Blind Validation Challenge
  4. Evaluating Models for Sub-Convective Pressure Fluctuations in Turbulent Boundary Layers
  5. Identification of Sources of Sub-Convective Wall Pressure Fluctuations Using Space-Time Pressure-Velocity Correlations
  6. Characterization of the Far-Wake of a Wall-Mounted Obstacle Embedded in a Turbulent Boundary Layer
  7. The Characteristics of Sub-Convective Wall Pressure Fluctuations in a Turbulent Boundary Layer
  8. Experimental Measurements on a Vortex Tube Separator Array
  9. Modeling the Surface Pressure Spectrum Beneath Turbulent Boundary Layers in Pressure Gradients
  10. Understanding the pressure fluctuations that arise within smooth surfaces subject to turbulent flows
  11. The Space-Time Correlation of Pressure Under High Reynolds Number Smooth Wall Turbulent Boundary Layers in Pressure Gradient Family
  12. Flow Field Features of the BEVERLI Hill Model
  13. The Effect of Grazing Flow on Pinhole Condenser Microphones
  14. RANS Simulations of Thermally Non-Uniform Supersonic Jets
  15. The Pressure Signature of High Reynolds Number Smooth Wall Turbulent Boundary Layers in Pressure Gradient Family
  16. Computational Fluid Dynamic Analysis for the Assessment of Experimental Design Risks and Flow Sensitivities for a Three-Dimensional Bump Flow
  17. Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows
  18. 250 kHz three-component Doppler velocimetry at 32 simultaneous points: a new capability for high speed flows
  19. Non-spherical particle size estimation using supervised machine learning
  20. Geometric scattering removal in cross-correlation Doppler global velocimetry by structured illumination
  21. In-flight thrust monitoring: an acoustics-based approach
  22. Use of Thermal Nonuniformity to Reduce Supersonic Jet Noise
  23. Turbine Engine Ingested Particle Monitoring: A Novel Application of Quantum Cascade IR Laser Extinction
  24. Mean Flow and Turbulence of a Heated Supersonic Jet with Temperature Nonuniformity
  25. Hybrid RANS/LES Turbulence Model Applied to a Transitional Unsteady Boundary Layer on Wind Turbine Airfoil
  26. Aerodynamic Analysis of Total Temperature Probe Thermal Performance Using Conjugate Heat Transfer
  27. Measurement Drift in 3-Hole Yaw Pressure Probes From 5 Micron Sand Fouling at 1050° C
  28. On the Application of Particle Image Velocimetry for Turbofan Engine Flow Quantification
  29. Laser Light Sheet Flow Visualization of the Space Launch System Booster Separation Test
  30. Three-Velocity-Component Cross-Correlation Doppler Global Velocimetry for the Space Launch System Booster Separation Test in the NASA Langley Unitary Plan Wind Tunnel
  31. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
  32. Laser velocimetry for turbofan inlet distortion applications
  33. Coupled velocity and temperature acoustic tomography in heated high subsonic mach number flows
  34. Filtered Rayleigh Scattering for Velocity and Temperature Measurements of a Heated Supersonic Jet with Thermal Non-Uniformity
  35. Space-time Description of the Density Near-field in a Non-uniformly Heated Jet.
  36. Statistical Flow Structures in Heated Supersonic Jets with Offset Temperature Non-Uniformities
  37. Synthesis of convection velocity and turbulence measurements in three-stream jets
  38. Investigation of velocity and temperature measurement sensitivities in cross-correlation filtered Rayleigh scattering (CCFRS)
  39. An experimental study on the coupling between adjacent Hartmann whistles
  40. Vortical flow development in round ducts across scales for engine inlet applications
  41. Laser Light Sheet Flow Visualization of the Space Launch System Booster Separation Test
  42. Three-Velocity-Component Cross-Correlation Doppler Global Velocimetry for the Space Launch System Booster Separation Test in the NASA Langley Unitary Plan Wind Tunnel
  43. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
  44. Distributed Anemometry via High-Definition Fiber Optic Sensing
  45. Demonstration of 250 kHz Three-Component Velocity Measurements using TRDGV at 32 Simultaneous Points
  46. Outdoor Acoustic Measurements of the Virginia Tech Heated Supersonic Jet Rig Using Ground Microphones
  47. Definition of Arbitrary Swirl Distortions by Solutions to the Helmholtz Equation
  48. Experimental Investigation on the Acoustic Field and Convection Velocity of Structures in a Heated Jet With Centered Thermal Non-Uniformity
  49. MOUNT INTERFERENCE EFFECTS ON TOTAL TEMPERATURE PROBES
  50. Experimental Investigation of the Very Near Pressure Field of a Heated Supersonic Jet with a Total Temperature Non-Uniformity
  51. The Flow and Turbulence Characteristics of a Heated Supersonic Jet with an Offset Total Temperature Non-Uniformity
  52. Turbofan Nose Cone Interactions With Inlet Swirl
  53. Enhanced Low-Order Model with Radiation for Total Temperature Probe Analysis and Design
  54. Complex Flow Generation and Development in a Full-Scale Turbofan Inlet
  55. Experimental Quantification of Fan Rotor Effects on Inlet Swirl Using Swirl Distortion Descriptors
  56. Nonintrusive Gas-Turbine Engine-Exhaust Characterization Using Acoustic Measurements
  57. Unsteady boundary layer development on a wind turbine blade: an experimental study of a surrogate problem
  58. StreamVane Turbofan Inlet Swirl Distortion Generator: Mean Flow and Turbulence Structure
  59. Cross-Correlation Doppler Global Velocimetry using Rayleigh and Mie Scattering
  60. Decomposition of Periodic Eddies with Varying Energy in a Turbulent Flow Using a Directional Averaging Technique
  61. Large-Eddy Simulations of Flow Control Effects of a DBD Plasma Actuator at Various Burst Frequencies on a Dynamic Flowfield around a Pitching NACA0012 Airfoil at Reynolds Number of 256,000
  62. Numerical Study of Transitional Unsteady Boundary Layer on Wind Turbine Airfoil Using Hybrid RANS/LES Turbulence Model
  63. Non-intrusive acoustic measurement of flow velocity and temperature in a high subsonic Mach number jet
  64. Enhanced Low-Order Model with Radiation for Total Temperature Probe Analysis and Design
  65. Computational Modeling of Total-Temperature Probes
  66. Experimental Quantification of Fan Rotor Effects on Inlet Swirl Using Swirl Distortion Descriptors
  67. Application of Proper Orthogonal Decomposition to High Speed Imaging for the Study of Combustion Oscillations
  68. Complex Flow Generation and Development in a Full-Scale Turbofan Inlet
  69. Synthesis of Convection Velocity and Turbulence Measurements in Three-Stream Jets for Investigation of Noise Sources
  70. Eddy Convection in Cold and Heated Supersonic Jets
  71. Experimental Investigation of a Heated Supersonic Jet with Total Temperature Non-Uniformity
  72. Extension of sonic anemometry to high subsonic Mach number flows
  73. Fan Rotor Flow Measurements in a Turbofan Engine Operating with Inlet Swirl Distortion
  74. Swirling Flow Evolution Part 2: StreamFlow 2D+t Model Validated with Stereo PIV Measurements
  75. Swirling Flow Evolution Part 1: Design and Stereo PIV Measurements at Select Planes
  76. Numerical and experimental study of the unsteady transitional boundary layer on a wind turbine airfoil
  77. Non-Intrusive Measurement of Gas Turbine Engine Exhaust Characteristics using Acoustic Measurements
  78. Fluctuating Pressure Gradients in Heated Supersonic Jets
  79. Scale-up of the Time-Resolved Doppler Global Velocimetry Technique
  80. Measurements of Fan Response to Inlet Total Pressure and Swirl Distortions Produced by Boundary Layer Ingesting Aircraft Configurations
  81. An overview of recent results using the StreamVane method for generating tailored swirl distortion in jet engine research
  82. A Hybrid Technique for Laser Flare Reduction
  83. Velocity Statistics and Spectra in Three-Stream Jets
  84. Eddy Convection in Developing Heated Supersonic Jets
  85. Computational Modeling of Radiation Effects on Total Temperature Probes
  86. Stereoscopic PIV measurements in a turbofan engine inlet with tailored swirl distortion
  87. A Diagnostic Technique for Particle Characterization Using Laser Light Extinction
  88. An Experimental Investigation of the Performance Impact of Swirl on a Turbine Exhaust Diffuser/Collector for a Series of Diffuser Strut Geometries
  89. Particle Image Velocimetry Applications Using Fluorescent Dye-doped Particles
  90. Fourth-order Spectral Statistics in the Developing Shear Layers of Hot Supersonic Jets
  91. The Experimental Studies of Improving the Aerodynamic Performance of a Turbine Exhaust System
  92. The Effect of Particle Lag on Supersonic Turbulent Boundary Layer Statistics
  93. Stereoscopic PIV Measurements of Swirl Distortion on a Full-Scale Turbofan Engine Inlet
  94. Spectral analysis of over-expanded cold jets via 3-component point Doppler velocimetry
  95. Time-Domain Cross-Correlation Scan DGV (CCS-DGV) for Mean-Velocity Boundary Layer Measurements
  96. Experimental Reynolds Stress Spectra in Hot Supersonic Round Jets
  97. Laser velocimetry with fluorescent dye-doped polystyrene microspheres
  98. A laser-Doppler velocimeter system for near-field velocity vector measurements in large facilities
  99. Novel Laser Doppler Acceleration Measurements of Particle Lag Through a Shock Wave
  100. A Laser-Based Optical Approach for Measuring Scour Depth around Hydraulic Structures