Use of pressure-sensitive paint for diagnostics in turbomachinery flows with shocks

Experiments in Fluids

Volumn 33, Issue 4, 2002, Pages 531-538

  Lepicovsky, J ^a   Bencic, T ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CALIBRATION; CHANNEL FLOW; FLOW VISUALIZATION; FLUTTER (AERODYNAMICS); LUMINOUS PAINT; REFLECTION; SUPERSONIC AERODYNAMICS;

PRESSURE-SENSITIVE PAINT;

TURBOMACHINERY;

EID: 0036806333     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-002-0476-x     Document Type: Article

References (19)

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