Shock-Dominated Flow
Shock-dominated flow is frequently encountered in high-speed aircraft and engines, and its flow characteristics directly determine the aerodynamic performance of the aircraft and engines. Due to the strong discontinuity and pressurization properties of shock waves, the shock-dominant flow exhibits s...
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| フォーマット: | Online |
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| 言語: | 英語 |
| 出版事項: |
MDPI - Multidisciplinary Digital Publishing Institute
2025
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| 主題: | |
| オンライン･アクセス: | ONIX_20250220_9783725820115_72 |
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| _version_ | 1869522449424449536 |
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| collection | Directory of Open Access Books |
| description | Shock-dominated flow is frequently encountered in high-speed aircraft and engines, and its flow characteristics directly determine the aerodynamic performance of the aircraft and engines. Due to the strong discontinuity and pressurization properties of shock waves, the shock-dominant flow exhibits strong non-linearity, strong inviscid–viscous interaction, and significant historical effects, making it difficult to predict the related flow structures and behaviors. With the development of aircraft towards higher speeds, better performance, and more intelligent control, shock-dominated flow is a key scientific issue, involving complex high-speed aerodynamics, flow stability, fluid–thermal structure–acoustic multi-fields interaction, flow control, and artificial intelligence. For this reason, this Special Issue focuses on the shock–boundary layer interaction, shock–shock interaction, shock–vortex interaction, shock oscillation, shock-dominated flow in high-speed aircraft/engines, computational fluid dynamics (CFD) and experimental methods in shock-dominated flow research, shock aerodynamic heating and cooling, shock–thermal structure interaction, etc. |
| format | Online |
| id | doab-20.500.12854ir-152708 |
| institution | Directory of Open Access Books |
| language | eng |
| publishDate | 2025 |
| publishDateRange | 2025 |
| publishDateSort | 2025 |
| publisher | MDPI - Multidisciplinary Digital Publishing Institute |
| publisherStr | MDPI - Multidisciplinary Digital Publishing Institute |
| record_format | ojs |
| spelling | doab-20.500.12854ir-1527082025-02-20T12:56:49Z Shock-Dominated Flow Huang, Hexia Tian, Ye Tan, Huijun dynamic micro-vortex generator shock wave/boundary layer interaction dynamic grid simulation flow control supersonic inlet shock wave/vortex muzzle jet constrained boundary reflection dynamic mesh cavity flows noise prediction delayed detached eddy overexpansion state flow separation single-expansion ramp nozzle (SERN) external flow numerical simulation hypersonic double compression corner shock wave/boundary interaction plasma actuation wind shear hypersonic inlet/isolator shock train unsteady simulation surface arc discharge experimental research micro-serration separation control dynamic mode decomposition spiked-blunt body flow unsteadiness high-speed schlieren spectral analysis initial jet shock wave vortex dynamic grid 3D n/a thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues thema EDItEUR::M Medicine and Nursing::MJ Clinical and internal medicine::MJC Diseases and disorders::MJCL Oncology Shock-dominated flow is frequently encountered in high-speed aircraft and engines, and its flow characteristics directly determine the aerodynamic performance of the aircraft and engines. Due to the strong discontinuity and pressurization properties of shock waves, the shock-dominant flow exhibits strong non-linearity, strong inviscid–viscous interaction, and significant historical effects, making it difficult to predict the related flow structures and behaviors. With the development of aircraft towards higher speeds, better performance, and more intelligent control, shock-dominated flow is a key scientific issue, involving complex high-speed aerodynamics, flow stability, fluid–thermal structure–acoustic multi-fields interaction, flow control, and artificial intelligence. For this reason, this Special Issue focuses on the shock–boundary layer interaction, shock–shock interaction, shock–vortex interaction, shock oscillation, shock-dominated flow in high-speed aircraft/engines, computational fluid dynamics (CFD) and experimental methods in shock-dominated flow research, shock aerodynamic heating and cooling, shock–thermal structure interaction, etc. 2025-02-20T12:56:46Z 2025-02-20T12:56:46Z 2024 book ONIX_20250220_9783725820115_72 9783725820115 9783725820122 https://directory.doabooks.org/handle/20.500.12854/152708 eng application/octet-stream Attribution 4.0 International https://mdpi.com/books/pdfview/book/9795 MDPI - Multidisciplinary Digital Publishing Institute 10.3390/books978-3-7258-2012-2 10.3390/books978-3-7258-2012-2 46cabcaa-dd94-4bfe-87b4-55023c1b36d0 9783725820115 9783725820122 212 Basel open access |
| spellingShingle | dynamic micro-vortex generator shock wave/boundary layer interaction dynamic grid simulation flow control supersonic inlet shock wave/vortex muzzle jet constrained boundary reflection dynamic mesh cavity flows noise prediction delayed detached eddy overexpansion state flow separation single-expansion ramp nozzle (SERN) external flow numerical simulation hypersonic double compression corner shock wave/boundary interaction plasma actuation wind shear hypersonic inlet/isolator shock train unsteady simulation surface arc discharge experimental research micro-serration separation control dynamic mode decomposition spiked-blunt body flow unsteadiness high-speed schlieren spectral analysis initial jet shock wave vortex dynamic grid 3D n/a thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues thema EDItEUR::M Medicine and Nursing::MJ Clinical and internal medicine::MJC Diseases and disorders::MJCL Oncology Shock-Dominated Flow |
| title | Shock-Dominated Flow |
| title_full | Shock-Dominated Flow |
| title_fullStr | Shock-Dominated Flow |
| title_full_unstemmed | Shock-Dominated Flow |
| title_short | Shock-Dominated Flow |
| title_sort | shock dominated flow |
| topic | dynamic micro-vortex generator shock wave/boundary layer interaction dynamic grid simulation flow control supersonic inlet shock wave/vortex muzzle jet constrained boundary reflection dynamic mesh cavity flows noise prediction delayed detached eddy overexpansion state flow separation single-expansion ramp nozzle (SERN) external flow numerical simulation hypersonic double compression corner shock wave/boundary interaction plasma actuation wind shear hypersonic inlet/isolator shock train unsteady simulation surface arc discharge experimental research micro-serration separation control dynamic mode decomposition spiked-blunt body flow unsteadiness high-speed schlieren spectral analysis initial jet shock wave vortex dynamic grid 3D n/a thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues thema EDItEUR::M Medicine and Nursing::MJ Clinical and internal medicine::MJC Diseases and disorders::MJCL Oncology |
| topic_facet | dynamic micro-vortex generator shock wave/boundary layer interaction dynamic grid simulation flow control supersonic inlet shock wave/vortex muzzle jet constrained boundary reflection dynamic mesh cavity flows noise prediction delayed detached eddy overexpansion state flow separation single-expansion ramp nozzle (SERN) external flow numerical simulation hypersonic double compression corner shock wave/boundary interaction plasma actuation wind shear hypersonic inlet/isolator shock train unsteady simulation surface arc discharge experimental research micro-serration separation control dynamic mode decomposition spiked-blunt body flow unsteadiness high-speed schlieren spectral analysis initial jet shock wave vortex dynamic grid 3D n/a thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues thema EDItEUR::M Medicine and Nursing::MJ Clinical and internal medicine::MJC Diseases and disorders::MJCL Oncology |
| url | ONIX_20250220_9783725820115_72 |