Study of the Flow Within Finite-Span Complex Cavities Using Particle Image Velocimetry and Pressure Sensitive Paint
Author:
Affiliation:
1. Sandia National Laboratories
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1474
Reference22 articles.
1. 2Ahuja, K. K. and Mendoza, J. “Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes,” Contractor Report 4653, NASA, 1995.
2. Effect of Planform Aspect Ratio on Flow Oscillations in Rectangular Cavities
3. Acoustic Resonances in a 2D High Lift Configuration and 3D Open Cavity
4. Three-dimensional effects of supersonic cavity flow due to the variation of cavity aspect and width ratios
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1. Fluid–Structure Interactions on a Tunable Store in Complex Cavity Flow;Journal of Aircraft;2019-07
2. Effects of Cavity Width on Resonance Dynamics using Planform Time-Resolved Particle Image Velocimetry;2018 AIAA Aerospace Sciences Meeting;2018-01-07
3. Effects of Cavity Width on Compressible Resonance Dynamics using Time-Resolved Pressure Sensitive Paint and Particle Image Velocimetry;47th AIAA Fluid Dynamics Conference;2017-06-02
4. Study of Fluid-Structure Interactions on a Tunable Store in Complex Cavity Flow;47th AIAA Fluid Dynamics Conference;2017-06-02
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