All Stories

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