Detection of fluctuating density gradient flow field in shock wave boundary layer interactions using laser Schlieren system

Experiments in Fluids

Volumn 32, Issue 4, 2002, Pages 527-531

  Verma, S B ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; BOUNDARY LAYER FLOW; CARBON DIOXIDE; HYPERSONIC FLOW; LASER APPLICATIONS; LASER BEAMS; SCHLIEREN SYSTEMS; SHOCK WAVES; STATISTICAL METHODS; TURBULENT FLOW;

FLUCTUATING DENSITY GRADIENT FLOW; LASER SCHLIEREN SYSTEM; SHOCK WAVE-BOUNDARY LAYER INTERACTION;

FLOW VISUALIZATION;

EID: 0036538122     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-001-0382-7     Document Type: Article

References (13)

1. Unsteadiness of the separation shock wave structure in a supersonic compression ramp field
2. The cross-beam correlation technique
3. Laser Schlieren cross-beam measurements in a supersonic jet shear layer
4. Unsteady pressure loads generated by swept shock-wave/boundary-layer interactions
5. Fluctuating wall pressure under a separated supersonic flow
6. Hypersonic flow over axially symmetric spiked bodies
7. Wide-angle light scattering in shock-laser interaction
8. Shock detection technique based on light scattering by shock
9. Comparison of hot-film probe and optical techniques for sensing shock motion
10. Real-time optical measurement of time-dependent shock position
11. Nature of shock-wave/boundary-layer interaction on a 24°ramp model
12. Study of flow unsteadiness in a hypersonic swbli flow field on an HAC model