Effects of Porous Gap Fillers on Leading-Edge Slat Noise of 30P30N. Part II: PIV Measurements
Author:
Affiliation:
1. Florida State University Florida Center for Advanced Aero Propulsion
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2987
Reference10 articles.
1. Zhang, Y., ONeill, A., Cattafesta, L. N., Pascioni, K., Choudhari, M., Khorrami, M. R., Lockard, D. P., and Turner, T. "AssessmentofNoiseReductionConceptsforLeading-EdgeSlatNoise,"2018AIAA/CEASAeroacousticsConference,American InstituteofAeronauticsandAstronautics,2018. https://doi.org/10.2514/6.2018-3461,AIAAPaper2018-3461.
2. Slat Noise Control Using a Slat Gap Filler
3. Investigation of the 30P30N Slat Flow Field with Passive Control Devices Using Particle Image Velocimetry
4. Assessment of Slat Extensions and a Cove Filler for Slat Noise Reduction
5. Aerodynamic and Aeroacoustic Experimentation of a Slat-Gap Filler for Airframe Noise Reduction
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1. Slat noise in high-lift systems;Progress in Aerospace Sciences;2024-04
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