All Stories

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