Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers
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| Title: | Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers |
|---|---|
| Description: | Experimental investigation in turbulent boundary layer flows represents one of the canonical geometries of wall bounded shear flows. Utmost relevance of such experiments, however, is applied in the engineering applications in aerospace and marine industries. In particular, continuous effort is being imparted to explore the underlying physics of the flow in order to develop models for numerical tools and to achieve flow control. Flow control experiments have been widely investigated since 1930's. Several flow control technique has been explored and have shown potential benefit. But the choice of control technique depends largely on the boundary condition and the type of application. Hence, friction drag of subsonic transport aircraft is intended to be reduced within the scope of this Ph. D. topic. Therefore, application of active control method such as microblowing effect in the incompressible, zero pressure gradient turbulent boundary layer was investigated. A series of experiments have been performed in two different wind tunnel facilities. Wind tunnel from Department of Aerodynamics and Fluid Mechanics (LAS) was used for the measurements for moderate Reynolds number range in co-operation with the wind tunnel from Laboratoire de M´ecanique de Feiret Lille for large Reynolds number range. Measurements are conducted with the help of state-of-the-art techniques such as Laser Doppler Anemometry, Particle Image Velocimetry and electronic pressure sensors. |
| Authors: | Hasanuzzaman, Gazi |
| Resource Type: | eBook. |
| Subjects: | Velocity modulation |
| Categories: | SCIENCE / Mechanics / Fluids, SCIENCE / Experiments & Projects, TECHNOLOGY & ENGINEERING / Sensors |
| Database: | eBook Collection (EBSCOhost) |
| FullText | Links: – Type: ebook-pdf Text: Availability: 0 |
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| Header | DbId: nlebk DbLabel: eBook Collection (EBSCOhost) An: 3163694 RelevancyScore: 1110 AccessLevel: 6 PubType: eBook PubTypeId: ebook PreciseRelevancyScore: 1109.74133300781 |
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| Items | – Name: Title Label: Title Group: Ti Data: Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers – Name: Abstract Label: Description Group: Ab Data: Experimental investigation in turbulent boundary layer flows represents one of the canonical geometries of wall bounded shear flows. Utmost relevance of such experiments, however, is applied in the engineering applications in aerospace and marine industries. In particular, continuous effort is being imparted to explore the underlying physics of the flow in order to develop models for numerical tools and to achieve flow control. Flow control experiments have been widely investigated since 1930's. Several flow control technique has been explored and have shown potential benefit. But the choice of control technique depends largely on the boundary condition and the type of application. Hence, friction drag of subsonic transport aircraft is intended to be reduced within the scope of this Ph. D. topic. Therefore, application of active control method such as microblowing effect in the incompressible, zero pressure gradient turbulent boundary layer was investigated. A series of experiments have been performed in two different wind tunnel facilities. Wind tunnel from Department of Aerodynamics and Fluid Mechanics (LAS) was used for the measurements for moderate Reynolds number range in co-operation with the wind tunnel from Laboratoire de M´ecanique de Feiret Lille for large Reynolds number range. Measurements are conducted with the help of state-of-the-art techniques such as Laser Doppler Anemometry, Particle Image Velocimetry and electronic pressure sensors. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Hasanuzzaman%2C+Gazi%22">Hasanuzzaman, Gazi</searchLink> – Name: TypePub Label: Resource Type Group: TypPub Data: eBook. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Velocity+modulation%22">Velocity modulation</searchLink> – Name: SubjectBISAC Label: Categories Group: Su Data: <searchLink fieldCode="ZK" term="%22SCIENCE+%2F+Mechanics+%2F+Fluids%22">SCIENCE / Mechanics / Fluids</searchLink><br /><searchLink fieldCode="ZK" term="%22SCIENCE+%2F+Experiments+%26+Projects%22">SCIENCE / Experiments & Projects</searchLink><br /><searchLink fieldCode="ZK" term="%22TECHNOLOGY+%26+ENGINEERING+%2F+Sensors%22">TECHNOLOGY & ENGINEERING / Sensors</searchLink> |
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| RecordInfo | BibRecord: BibEntity: Classifications: – Code: 621.38151 Scheme: ddc Type: prePub Languages: – Code: eng Text: English Subjects: – SubjectFull: Velocity modulation Type: general Titles: – TitleFull: Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Hasanuzzaman, Gazi – PersonEntity: Name: NameFull: Hasanuzzaman, Gazi IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 01 Type: published Y: 2022 – D: 30 M: 07 Type: profile Y: 2025 Identifiers: – Type: isbn-print Value: 9783736975583 – Type: isbn-electronic Value: 9783736965584 Titles: – TitleFull: Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers Type: main |
| ResultId | 1 |
