The wake imaging system (WIS) for rapid mappings of wind tunnel model flowfields is described and a summary of recent results is presented. Three different types of systems are discussed. These are: In addition, progress toward developing a low intrusive WIS for high-pressure transonic wind tunnels and for flight test applications is described.
Wake Imaging System Applications at the Boeing Aerodynamics Laboratory
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1985
1985-10-01
Conference paper
English
Application of Uncertainty Methodology at the Boeing Aerodynamics Laboratory
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