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PIV
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Towards In-Flight Measurements of Helicopter Blade Tip Vortices
Tip-Vortex Dynamics of a Pitching Rotor Blade-Tip Model
Starting Process of a Pulsed Jet as Seen by Schlieren Measurements
Flight-Testing Stability and Controllability of Otto Lilienthal’s Monoplane Design from 1893
Analysis of Dynamic Stall Using Dynamic Mode Decomposition Technique
Blade-Tip Vortex Detection in Maneuvering Flight Using the Background-Oriented Schlieren Technique
Blade Tip Vortex System of a Rotor with Cyclic Pitch
Dynamic Stall Control by Passive Disturbance Generators
Contributions of Particle Image Velocimetry to Helicopter Aerodynamics
Tip-Vortex Investigation on a Rotating and Pitching Rotor Blade
Experimental aspects of PIV applied to a Bo 105 helicopter in hover-flight condition.
Investigation of unsteady flow development over a pitching airfoil by means of TR-PIV
Aperiodicity in the near field of full-scale rotor blade tip vortices