Anodized aluminum pressure sensitive paint for short duration testing

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference

Volumn , Issue , 2002, Pages

  Sakaue, Hirotaka ^a   Matsumura, Shin ^a   Schneider, Steven P ^a   Sullivan, John P ^a  

^a Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC FLOW; INTAKE SYSTEMS; LUMINOUS PAINT; RAMJET ENGINES; SUPERSONIC AERODYNAMICS;

ANODIZED ALUMINUM PRESSURE SENSITIVE PAINTS; AXISYMMETRIC; LUDWIEG TUBE; MODEL SURFACE; SCRAMJET INLETS; SHORT DURATION TESTING; SURFACE PRESSURES; UNCERTAINTY ESTIMATION;

PAINT;

EID: 85087188905     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2908     Document Type: Conference Paper

References (17)

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