Add to ORKGDuring a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was investigated by means of stereoscopic BO
Measurements in the wake of a free-flying full-scale helicopter in ground effect were performed for ...
A series of comprehensive flight tests investigated the flight dynamics and explored the flight enve...
A series of comprehensive flight tests investigated the flight dynamics and explored the flight enve...
During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was inv...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
In this paper we present the application of a novel schlieren technique for two different helicopter...
Blade tip vortices and their interaction with the helicopter blades play an important role in the ge...
Interactions between blade tip vortices and the structural components of a helicopter play an import...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade t...
In this paper we present a novel measurement technique based on the refractive index variation in a ...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade-...
The background oriented Schlieren (BOS) technique was used to visualize the blade tip vortices of a ...
The present work discusses a methodology to reconstruct three-dimensional positions of rotor blade t...
Blade-tip vortices and their interaction with the helicopter blades play an important role in the ge...
Measurements in the wake of a free-flying full-scale helicopter in ground effect were performed for ...
Measurements in the wake of a free-flying full-scale helicopter in ground effect were performed for ...
A series of comprehensive flight tests investigated the flight dynamics and explored the flight enve...
A series of comprehensive flight tests investigated the flight dynamics and explored the flight enve...
During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was inv...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
In this paper we present the application of a novel schlieren technique for two different helicopter...
Blade tip vortices and their interaction with the helicopter blades play an important role in the ge...
Interactions between blade tip vortices and the structural components of a helicopter play an import...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade t...
In this paper we present a novel measurement technique based on the refractive index variation in a ...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade-...
The background oriented Schlieren (BOS) technique was used to visualize the blade tip vortices of a ...
The present work discusses a methodology to reconstruct three-dimensional positions of rotor blade t...
Blade-tip vortices and their interaction with the helicopter blades play an important role in the ge...
Measurements in the wake of a free-flying full-scale helicopter in ground effect were performed for ...
Measurements in the wake of a free-flying full-scale helicopter in ground effect were performed for ...
A series of comprehensive flight tests investigated the flight dynamics and explored the flight enve...
A series of comprehensive flight tests investigated the flight dynamics and explored the flight enve...