Wake Imaging System Applications at the Boeing Aerodynamics Laboratory
851895
10/01/1985
- Event
- Content
- 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:
- Photographic WIS in low-speed wind tunnels.
- Computer graphics WIS in transonic wind tunnels.
- Flying strut traverser for large low-speed wind tunnels.
In addition, progress toward developing a low intrusive WIS for high-pressure transonic wind tunnels and for flight test applications is described.
- Pages
- 20
- Citation
- Crowder, J., "Wake Imaging System Applications at the Boeing Aerodynamics Laboratory," SAE Technical Paper 851895, 1985, https://doi.org/10.4271/851895.