Multisensor hot wire vorticity probe measurements of the formation field of two corotating vortices

Flow, Turbulence and Combustion

Volumn 83, Issue 2, 2009, Pages 153-183

  Romeos, Alexandros ^a   Lemonis, Georgios ^b   Panidis, Thrassos ^a   Papailiou, Demos D ^a  

^a UNIVERSITY OF PATRAS   (Greece)

^b Hellenic Aerospace Industry Corporation   (Greece)

Author keywords

Co rotating vortices; Hot wire anemometry (HWA); Multi sensor HWA; Tip vortex; Vorticity

Indexed keywords

ANGLES OF ATTACK; CO-ROTATING VORTICES; CROSS-PLANE FLOW; EXPERIMENTAL EVIDENCE; FIRST ORDER; FLOW FILED; FLUID SHEET; FLUID STREAMS; FORWARD DIFFERENCE SCHEME; HOT WIRE ANEMOMETRY; HOT WIRE ANEMOMETRY (HWA); HOT WIRES; MULTI SENSOR; MULTI-SENSOR HWA; NEAR WAKE; SEPARATION DISTANCES; SIMULTANEOUS MEASUREMENT; SPATIAL VELOCITY; STAGNATION POINTS; STREAMWISE VELOCITY; TEMPORAL CHANGE; THREE-DIMENSIONAL VECTORS; THREE-DIMENSIONAL VELOCITY; TIP VORTEX; VORTEX FORMATION; VORTICITY PROBE; WING CONFIGURATIONS; WIRE VELOCITY;

AERODYNAMICS; AIR; ANEMOMETERS; COMPUTATIONAL FLUID DYNAMICS; FLOW FIELDS; LOCATION; PRESSURE GRADIENT; PROBES; ROTATION; SENSOR ARRAYS; THREE DIMENSIONAL; VELOCITY; VELOCITY MEASUREMENT; VORTICITY; WAKES; WIND TUNNELS; WINGS; WIRE;

VORTEX FLOW;

EID: 68949213749     PISSN: 13866184     EISSN: 15731987     Source Type: Journal    
DOI: 10.1007/s10494-008-9193-8     Document Type: Article

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