Application of stereoscopic PIV to helicopter rotor blade tip vortices

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn , Issue , 2003, Pages 179-189

  Kato, Hiroyuki ^a,b   Watanabe, Shigeya ^a,b   Kondo, Natsuki ^a,c   Saito, Shigeru ^a,c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Wind Tunnel Technology Center   (Japan)

^c Fluid Science Research Center   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BLADE-VORTEX INTERACTION (BIV); IMAGE ACQUISITION; PARTICLE IMAGE VELOCIMETRY (PIV);

ACOUSTIC NOISE; CAMERAS; CHARGE COUPLED DEVICES; COMPUTATIONAL FLUID DYNAMICS; FLOW VISUALIZATION; HELICOPTER ROTORS; IMAGE ANALYSIS; SPECIAL EFFECTS; TURBOMACHINE BLADES; TURBULENCE; VELOCITY MEASUREMENT; VORTEX FLOW; WIND TUNNELS;

AERODYNAMICS;

EID: 1642520022     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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