Application of pressure-sensitive paint in supersonic nozzle research

Journal of Aircraft

Volumn 33, Issue 6, 1996, Pages 1109-1114

  Cler, Daniel ^a,d   Lamb, Milton ^a,d   Farokhi, Saeed ^b,d   Taghavi, Ray ^b,d   Hazlewood, Richard ^b,c,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b University of Kansas   (United States)

^c Aircraft Engineering   (United States)

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC PRESSURE; LUMINESCENCE; PAINT; PRESSURE MEASUREMENT; SUPERSONIC FLOW; VORTEX FLOW; WIND TUNNELS;

LUMINOPHORES; PRESSURE SENSITIVE PAINT TECHNIQUE; STERN-VOLMER RELATION; SUPERSONIC CAVITY RAMP VORTEX GENERATORS; SUPERSONIC NOZZLE; SURFACE PRESSURE DISTRIBUTION;

NOZZLES;

EID: 0030287598     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47064     Document Type: Article

References (16)

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