Zhang et al., 2024 - Google Patents
Slat noise in high-lift systemsZhang et al., 2024
- Document ID
- 5467951248858036874
- Author
- Zhang Y
- Cattafesta L
- Pascioni K
- Choudhari M
- Publication year
- Publication venue
- Progress in Aerospace Sciences
External Links
Snippet
This paper reviews several decades' worth of research on the topic of slat noise arising from high-lift systems of commercial aircraft. A high-lift system is commonly used for providing additional lift by deploying the leading-edge slat (s) and trailing-edge flap (s) during the …
- 238000013459 approach 0 abstract description 33
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
- Y02T50/16—Drag reduction by influencing airflow
- Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/12—Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Teruna et al. | Noise reduction mechanisms of an open-cell metal-foam trailing edge | |
Chong et al. | Self-noise produced by an airfoil with nonflat plate trailing-edge serrations | |
Lockard et al. | Noise radiation from a leading-edge slat | |
Zhang | Aircraft noise and its nearfield propagation computations | |
Chen et al. | Noise control for high-lift devices by slat wall treatment | |
Ricciardi et al. | Numerical noise prediction and source identification of a realistic landing gear | |
Zhang et al. | Slat noise in high-lift systems | |
Ananthan et al. | Trailing edge noise reduction using bio-inspired finlets | |
Lockard et al. | Noise simulations of the high-lift common research model | |
Li et al. | On the mechanism of acoustic resonances from a leading-edge slat | |
Nagy et al. | Aeroacoustics research in Europe: The CEAS-ASC report on 2020 & 2021 highlights | |
Gorji-Bandpy et al. | Airframe noise sources and reduction technologies in aircraft | |
Lockard et al. | The variation of slat noise with Mach and Reynolds numbers | |
Schram et al. | Aeroacoustics research in Europe: The CEAS-ASC report on 2022 highlights | |
Appelbaum et al. | Airframe noise simulations of a full-scale aircraft | |
Chen et al. | Effects of slat track on the flow and acoustic field of high-lift devices | |
Joslin et al. | Synergism of flow and noise control technologies | |
Hardin et al. | Prediction of airframe noise | |
Lockard et al. | Assessment of aeroacoustic simulations of the high-lift common research model | |
Ferris et al. | Simulations of a full-scale aircraft with installed airframe noise reduction technologies | |
Doshi et al. | Toward a passive control strategy for a supersonic multi-stream flow using resolvent analysis | |
Bai et al. | Noise characteristic of the nacelle/pylon/slat juncture in a realistic high-lift aircraft configuration | |
Housman et al. | Slat noise predictions using higher-order finite-difference methods on overset grids | |
Murayama et al. | Noise Reduction Design for Flap Side-edges toward FQUROH Flight Demonstration | |
Murayama et al. | Airframe noise reduction of flap side-edge using vortex generators |