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100%: Liu, Chaoqun/ Li, Qin/ Yan, Yonghua/ Yang, Yong/ Yang, Guang/ Dong, Xiangrui: High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (Frontiers in Aerospace Science) (ISBN: 9781681085982) 2017, Bentham Science Publishers, in Englisch, Taschenbuch.Nur diese Ausgabe anzeigen…
100%: Chaoqun Liu, Qin Li, Yonghua Yan, Yong Yang, Guang Yang, Xiangrui Dong: High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (Frontiers in Aerospace Science Book 2) (ISBN: 9781681085975) in Englisch, auch als eBook.Nur diese Ausgabe anzeigen…
High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (Frontiers in Aerospace Science)
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Bester Preis: € 103,50 (vom 18.02.2018)1
High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (Frontiers in Aerospace Science) (2017)
EN PB NWISBN: 9781681085982 bzw. 1681085984, in Englisch, 320 Seiten, Bentham Science Publishers, Taschenbuch, neu.
Lieferung aus: Vereinigte Staaten von Amerika, Usually ships in 24 hours, free shipping for AmazonPrime only. Regular USD 4.98.
Von Händler/Antiquariat, Amazon.com.
This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ramp flows with and without control at Mach 2.5 and Re=5760. Flow control in the form of microramp vortex generators (MVG) is applied. The results show that a MVG can distinctly reduce the separation zone at the ramp corner and lower the boundary layer shape factor under simulated conditions. A series of new findings about the MVG-ramp flow are obtained, including structures relevant to surface pressure, three-dimensional structures of the re-compression shock waves, a complete surface separation pattern, momentum deficit and a new secondary vortex system. A new mechanism of shock-boundary layer interaction control by MVG associated with a series of vortex rings is also presented. Vortex rings strongly interact with air flow and play an important role in the separation zone reduction. Additionally, readers will learn about the governing equation, boundary condition, high quality grid generation, high order shock capturing scheme and DNS inflow condition in detail. This volume will, therefore, serve as a useful reference for aerospace researchers using LES methods to study shock boundary layer interaction and supersonic flow control. Paperback, Label: Bentham Science Publishers, Bentham Science Publishers, Product group: Book, Published: 2017-12-11, Studio: Bentham Science Publishers, Sales rank: 3226896.
Von Händler/Antiquariat, Amazon.com.
This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ramp flows with and without control at Mach 2.5 and Re=5760. Flow control in the form of microramp vortex generators (MVG) is applied. The results show that a MVG can distinctly reduce the separation zone at the ramp corner and lower the boundary layer shape factor under simulated conditions. A series of new findings about the MVG-ramp flow are obtained, including structures relevant to surface pressure, three-dimensional structures of the re-compression shock waves, a complete surface separation pattern, momentum deficit and a new secondary vortex system. A new mechanism of shock-boundary layer interaction control by MVG associated with a series of vortex rings is also presented. Vortex rings strongly interact with air flow and play an important role in the separation zone reduction. Additionally, readers will learn about the governing equation, boundary condition, high quality grid generation, high order shock capturing scheme and DNS inflow condition in detail. This volume will, therefore, serve as a useful reference for aerospace researchers using LES methods to study shock boundary layer interaction and supersonic flow control. Paperback, Label: Bentham Science Publishers, Bentham Science Publishers, Product group: Book, Published: 2017-12-11, Studio: Bentham Science Publishers, Sales rank: 3226896.
2
High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (Frontiers in Aerospace Science Book 2) (2018)
EN NW EB DLISBN: 9781681085975 bzw. 1681085976, in Englisch, 420 Seiten, Bentham Science Publishers, neu, E-Book, elektronischer Download.
Lieferung aus: Vereinigte Staaten von Amerika, ebook for download, Free shipping.
This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ramp flows with and without control at Mach 2.5 and Re=5760. Flow control in the form of microramp vortex generators (MVG) is applied. The results show that a MVG can distinctly reduce the separation zone at the ramp corner and lower the boundary layer shape factor under simulated conditions. A series of new findings about the MVG-ramp flow are obtained, including structures relevant to surface pressure, three-dimensional structures of the re-compression shock waves, a complete surface separation pattern, momentum deficit and a new secondary vortex system. A new mechanism of shock-boundary layer interaction control by MVG associated with a series of vortex rings is also presented. Vortex rings strongly interact with air flow and play an important role in the separation zone reduction. Additionally, readers will learn about the governing equation, boundary condition, high quality grid generation, high order shock capturing scheme and DNS inflow condition in detail. This volume will, therefore, serve as a useful reference for aerospace researchers using LES methods to study shock boundary layer interaction and supersonic flow control. Kindle Edition, Format: Kindle eBook, Label: Bentham Science Publishers, Bentham Science Publishers, Product group: eBooks, Published: 2018-01-29, Release date: 2018-01-29, Studio: Bentham Science Publishers.
This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ramp flows with and without control at Mach 2.5 and Re=5760. Flow control in the form of microramp vortex generators (MVG) is applied. The results show that a MVG can distinctly reduce the separation zone at the ramp corner and lower the boundary layer shape factor under simulated conditions. A series of new findings about the MVG-ramp flow are obtained, including structures relevant to surface pressure, three-dimensional structures of the re-compression shock waves, a complete surface separation pattern, momentum deficit and a new secondary vortex system. A new mechanism of shock-boundary layer interaction control by MVG associated with a series of vortex rings is also presented. Vortex rings strongly interact with air flow and play an important role in the separation zone reduction. Additionally, readers will learn about the governing equation, boundary condition, high quality grid generation, high order shock capturing scheme and DNS inflow condition in detail. This volume will, therefore, serve as a useful reference for aerospace researchers using LES methods to study shock boundary layer interaction and supersonic flow control. Kindle Edition, Format: Kindle eBook, Label: Bentham Science Publishers, Bentham Science Publishers, Product group: eBooks, Published: 2018-01-29, Release date: 2018-01-29, Studio: Bentham Science Publishers.
3
High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (2017)
EN NW EB DLISBN: 9781681085975 bzw. 1681085976, in Englisch, Bentham Science Publishers, Bentham Science Publishers, Bentham Science Publishers, neu, E-Book, elektronischer Download.
Lieferung aus: Australien, in-stock.
This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ramp flows with and without control at Mach 2.5 and.
This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ramp flows with and without control at Mach 2.5 and.
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High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator (Frontiers in Aerospace Science) (2017)
EN PB NWISBN: 9781681085982 bzw. 1681085984, in Englisch, Bentham Science Publishers, Taschenbuch, neu.
Von Händler/Antiquariat, Revaluation Books [2134736], Exeter, United Kingdom.
320 pages. 10.00x7.00x0.76 inches. In Stock.
320 pages. 10.00x7.00x0.76 inches. In Stock.
5
High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator
EN NW EBISBN: 9781681085982 bzw. 1681085984, in Englisch, Bentham Science Publishers, neu, E-Book.
Lieferung aus: Vereinigte Staaten von Amerika, Ebook for download.
Technology, No Description Available, eBook.
Technology, No Description Available, eBook.
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