Pressure-sensitive paint application to a wing-body model in a hypersonic shock tunnel

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference

Volumn , Issue , 2002, Pages

  Nakakita, Kazuyuki ^a   Asai, Keisuke ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; LUMINOUS PAINT; SHOCK WAVES; SUPERSONIC AERODYNAMICS; WIND TUNNELS; WINGS;

ANGLES OF ATTACK; ANODIZED ALUMINUM PRESSURE SENSITIVE PAINTS; COMPLICATED GEOMETRY; EFFECTS OF TEMPERATURE; HYPERSONIC WIND TUNNELS; PRESSURE SENSITIVE PAINTS; QUANTITATIVE AGREEMENT; STRONG INTERACTION;

PAINT;

EID: 84995746407     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2911     Document Type: Conference Paper

References (17)

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