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- W3202293633 abstract "From past 50 years of research shock wave boundary interaction (SBLI) has played the most crucial role while designing the Air vehicle (like Rocket, Airplane, Missile, etc.,). Here considering ten different papers and deeply understanding the concept and reviewing the literature. The shock wave boundary layer interaction has various kinds of usages in the aerospace industry (like transonic and supersonic flight vehicle surfaces, and surfaces of rockets, missiles, transonic turbine blade passages, and re-entry vehicles, transonic gas turbine blade tip gaps, scramjet isolator ducts, supersonic aircraft engine intakes). Considering various applications mentioned above and taking the research paper for each application and reviewed which has been done in the paper through which medium. Considering the numerical method to determine the concept of shock boundary layer interaction (SBLI) and comparing the result with CFD to provide the data that attain in an efficient manner. And Conducting experiments through different wind tunnels (like LENS XX, transonic and supersonic wind tunnel) and comparing the result with CFD. Determining the dimension flow while conducting the experiment. Shock wave boundary layer interaction (SBLI) review based on different concepts of interacting profiles in different boundary-layer conditions on different models and applications." @default.
- W3202293633 created "2021-10-11" @default.
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- W3202293633 date "2021-09-01" @default.
- W3202293633 modified "2023-09-22" @default.
- W3202293633 title "A Review on Effect of Shock Wave Boundary Layer Interaction in different Flows Fields" @default.
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