All Stories

  1. Application of BOS velocimetry to full-scale helicopter flight tests
  2. Experiments and Modeling of a Single Multicopter Rotor Response to Sinusoidal Vertical Gusts
  3. BOS and Hot-Film Analysis of a CH-53G Helicopter Wake in Ground Effect
  4. Projected moving patterns for reference-free background-oriented schlieren technique (BOS)
  5. Special issue on advances in rotorcraft research and technology
  6. Application of BOS Velocimetry to Full-scale Helicopter Flight Tests
  7. Experiments and Modelling of Multicopter Rotor Response to Sinusoidal Vertical Gusts
  8. Experimental and Computational Investigation of Aerodynamic Interactions in Quadrotor Configurations
  9. Enhancing numerical accuracy in the prediction of rotor wake vortex structures
  10. Experimental investigation of UAV rotor aeroacoustics and aerodynamics with computational cross-validation
  11. BOS and Hot-Film Analysis of a CH-53G Helicopter Wake in Ground Effect
  12. Experimental Investigation of Quadrotor Aerodynamics with Computational Cross-Validation
  13. Numerical and Experimental Assessment of Parameters Influencing the Development of Secondary Vortex Structures in Rotor Wakes
  14. Review of rotating wing dynamic stall: Experiments and flow control
  15. Evaluation of Pilot Assistance Systems for Helicopter Ship Deck Landing
  16. Development of secondary vortex structures in rotor wakes
  17. Boundary Layer Transition Measured by DIT on the PSP Rotor in Forward Flight
  18. Infrared thermography for boundary layer transition measurements
  19. Transition measurements of upper and lower rotor blade surfaces in forward flight
  20. Thermographic flow visualization by means of non-negative matrix factorization
  21. Reference-free digital shadowgraphy using a moving BOS background
  22. Effect of the Model-Sidewall Connection for a Dynamic Stall Airfoil Experiment
  23. Helicopter Rotor Boundary Layer Transition Measurement in Forward Flight Using an Infrared Camera
  24. Review of measurement techniques for unsteady helicopter rotor flows
  25. Experimental study of secondary vortex structures in a rotor wake
  26. Advanced infrared thermography data analysis for unsteady boundary layer transition detection
  27. Dynamic Stall Computations of Double-Swept Rotor Blades
  28. Unsteady Boundary Layer Transition Detection with Local Infrared Thermography
  29. Effect of Sweep on a Pitching Finite Wing
  30. Optimization of differential infrared thermography for unsteady boundary layer transition measurement
  31. On the Effect of Rotational Forces on Rotor Blade Boundary-Layer Transition
  32. A Novel Experiment to Understand the Dynamic Stall Phenomenon in Rotor Axial Flight
  33. Numerical Investigations of Dynamic Stall on a Rotor with Cyclic Pitch Control
  34. Tip-Vortex Investigation on a Rotating and Pitching Rotor Blade
  35. Correction to: Numerical investigation of blade-tip-vortex dynamics
  36. Numerical investigation of blade-tip-vortex dynamics
  37. On the Effect of Rotational Forces on Rotor Blade Boundary-Layer Transition
  38. Influence of a back-flow flap on the dynamic stall flow topology
  39. Unsteady Boundary Layer Transition Detection by Automated Analysis of Hot Film Data
  40. Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb
  41. Numerical Simulation of an Adaptive Wall in a Virtual Transonic Wind Tunnel
  42. Analysis of differential infrared thermography for boundary layer transition detection
  43. Dynamic Stall Simulations on a Pitching Finite Wing
  44. Rotating Blade Stall Maps Measured by Differential Infrared Thermography
  45. Reduction of dynamic stall using a back-flow flap
  46. A new method of dynamic and static stall detection using infrared thermography
  47. Dynamic Stall Simulations on a Pitching Finite Wing
  48. Detection of Unsteady Boundary Layer Transition Using Three Experimental Methods
  49. Comparison Between Two-Dimensional and Three-Dimensional Dynamic Stall
  50. Transition Determination on a Periodic Pitching Airfoil Using Phase Averaging of Pressure Data
  51. Numerical Investigation of Three-Dimensional Static and Dynamic Stall on a Finite Wing
  52. Boundary layer transition determination for periodic and static flows using phase-averaged pressure data
  53. Boundary-layer transition on a rotor blade measured by temperature-sensitive paint, thermal imaging and image derotation
  54. Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
  55. Analysis of Dynamic Stall Using Dynamic Mode Decomposition Technique
  56. Investigation of three-dimensional dynamic stall on an airfoil using fast-response pressure-sensitive paint
  57. Starting Process of a Pulsed Jet as Seen by Schlieren Measurements
  58. Experimental Investigation of Air Jets to Control Shock-Induced Dynamic Stall
  59. Aerodynamic and structural investigation of an active back-flow flap for dynamic stall control
  60. Experimental investigation of high-pressure pulsed blowing for dynamic stall control
  61. An active back-flow flap for a helicopter rotor blade
  62. Numerical Investigations of a Back-Flow Flap for Dynamic Stall Control
  63. Experimental Investigation of Unsteady Transition on a Pitching Rotor Blade Airfoil
  64. Numerical Investigation of the Influence of the Model Installation on Rotor Blade Airfoil Measurements
  65. Influence of Rotation on Dynamic Stall
  66. Analysis of Dynamic Stall using Dynamic Mode Decomposition Technique
  67. Effect of the Model-Sidewall Connection for a Static Airfoil Experiment
  68. Investigation of Aero-Optical Effects in Model Deformation Measurements in a Transonic Flow
  69. Numerical Investigation of Pulsed Air Jets for Dynamic Stall Control on the OA209 Airfoil
  70. Experimental Investigation of Air Jets for the Control of Compressible Dynamic Stall
  71. Experimental Investigation of Dynamic Stall Performance for the EDI-M109 and EDI-M112 Airfoils
  72. Numerical Comparison of Dynamic Stall for Two-Dimensional Airfoils and an Airfoil Model in the DNW–TWG
  73. Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods
  74. Numerical investigation of air jets for dynamic stall control on the OA209 airfoil
  75. Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experiment
  76. Comparison of Supersonic Combustion Tests with Shock Tunnels, Flight and CFD
  77. Ground testing of the HyShot supersonic combustion flight experiment in HEG
  78. Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data
  79. Upstream porthole injection in a 2-D scramjet model
  80. Simulation of Oscillating Airfoils and Moving Flaps Employing the DLR-TAU Unsteady Grid Adaptation