Rayleigh imaging and flow tagging in ground test facilities
Abstract
The authors present preliminary results on the application of ultraviolet Rayleigh imaging and RELIEF flow tagging to a high Reynolds number, Mach 3 blow-down air facility at Princeton University's Gas Dynamics Laboratory. RELIEF tagging was accomplished using stimulated Raman scattering to vibrationally excite oxygen molecules. Examples include instantaneous images of boundary-layer structure and shock-wave/boundary-layer interactions, as well as very recent results of flow tagging velocity measurements in the free-stream and boundary-layer regions of this facility. The future implementation of filtered Rayleigh scattering is also discussed.
- Publication:
-
ICIASF 1991 1- 14th International Congress on Instrumentation in Aerospace Simulation Facilities
- Pub Date:
- 1991
- Bibcode:
- 1991icia.cong..255M
- Keywords:
-
- Boundary Layers;
- Flow Measurement;
- Flow Visualization;
- Rayleigh Scattering;
- Supersonic Wind Tunnels;
- Velocity Measurement;
- Ground Tests;
- Shock Waves;
- Instrumentation and Photography