Data fusion in wind tunnel testing; Combined pressure paint and model deformation measurements (Invited)

20th AIAA Advanced Measurement and Ground Testing Technology Conference

Volumn , Issue , 1998, Pages

  Bell, James H ^a   Burner, Alpheus W ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DATA FUSION; DEFORMATION; PAINT; WIND STRESS;

BENEFIT TO COST RATIOS; DEFORMATION MEASUREMENTS; MODEL DEFORMATIONS; OPTICAL TECHNIQUE; PRESSURE SENSITIVE PAINTS; WIND TUNNEL MEASUREMENTS; WIND TUNNEL TESTS; WIND-TUNNEL TESTING;

WIND TUNNELS;

EID: 84982318546     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

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3. McLachlan, E.G., Bell, J.H. 1995 Pressure-Sensitive Paint in Aerodynamic Testing. Exp. Thermal and Fluid Science, vol. 10, pp. 470-485.
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