An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Slanted Slots

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Total Pages : pages
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Book Synopsis An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Slanted Slots by : A. Hamed

Download or read book An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Slanted Slots written by A. Hamed and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Normal and Slanted Slots

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Normal and Slanted Slots by : A. Hamed

Download or read book An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Normal and Slanted Slots written by A. Hamed and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction

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ISBN 13 :
Total Pages : 916 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction by : C. C. Sun

Download or read book An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction written by C. C. Sun and published by . This book was released on 1977 with total page 916 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tabulated data from a series of experimental studies of the interaction of a shock wave with a turbulent boundary layer in axisymmetric flow configurations is presented. The studies were conducted at the walls of circular wind tunnels and on the cylindrical centerbody of an annular flow channel. Detailed pitot pressure profiles and wall static pressure profiles upstream of, within and downstream of the interaction region are given. Results are presented for flows at nominal freestream Mach Numbers of 2, 3 and 4. For studies at the tunnel sidewalls, the shock waves were produced by conical shock generators mounted on the centerline of the wind tunnel at zero angle of attack. The annular ring generator was used to produce the shock wave at the centerbody of the annular flow channel. The effects of boundary layer bleed were examined in the investigation. Both bleed rate and bleed location were studied. Most of the bleed studies were conducted with bleed holes drilled normal to the wall surface but the effects of slot suction were also examined. A summary of the principal results and conclusions is given.

Shock Wave-Boundary-Layer Interactions

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Publisher : Cambridge University Press
ISBN 13 : 1139498649
Total Pages : 481 pages
Book Rating : 4.1/5 (394 download)

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Book Synopsis Shock Wave-Boundary-Layer Interactions by : Holger Babinsky

Download or read book Shock Wave-Boundary-Layer Interactions written by Holger Babinsky and published by Cambridge University Press. This book was released on 2011-09-12 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.

Experimental Investigation of Crossing Shock Wave-Turbulent Boundary Layer-Bleed Interaction

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ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of Crossing Shock Wave-Turbulent Boundary Layer-Bleed Interaction by : Hyun D. Kim

Download or read book Experimental Investigation of Crossing Shock Wave-Turbulent Boundary Layer-Bleed Interaction written by Hyun D. Kim and published by . This book was released on 1996 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flowfield Measurements in a Slot-Bled Oblique Shock Wave and Turbulent Boundary-Layer Interaction

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ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flowfield Measurements in a Slot-Bled Oblique Shock Wave and Turbulent Boundary-Layer Interaction by :

Download or read book Flowfield Measurements in a Slot-Bled Oblique Shock Wave and Turbulent Boundary-Layer Interaction written by and published by . This book was released on 1998 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Crossing Shock Wave-turbulent Boundary Layer-bleed Interaction

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ISBN 13 :
Total Pages : 9 pages
Book Rating : 4.:/5 (956 download)

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Book Synopsis Experimental Investigation of Crossing Shock Wave-turbulent Boundary Layer-bleed Interaction by : Hyun Dae Kim

Download or read book Experimental Investigation of Crossing Shock Wave-turbulent Boundary Layer-bleed Interaction written by Hyun Dae Kim and published by . This book was released on 1996 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theoretical Investigation of 3-D Shock Wave-turbulent Boundary Layer Interactions

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Publisher :
ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Theoretical Investigation of 3-D Shock Wave-turbulent Boundary Layer Interactions by : Doyle D. Knight

Download or read book Theoretical Investigation of 3-D Shock Wave-turbulent Boundary Layer Interactions written by Doyle D. Knight and published by . This book was released on 1988 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1994 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves

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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves by : Earl C. Watson

Download or read book Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves written by Earl C. Watson and published by . This book was released on 1969 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar and turbulent boundary layer interactions with externally generated shock waves.

An Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in Axially Symmetric Internal Flow Including the Effects of Mass Bleed

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ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.:/5 (976 download)

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Book Synopsis An Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in Axially Symmetric Internal Flow Including the Effects of Mass Bleed by : William Russell Seebaugh

Download or read book An Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in Axially Symmetric Internal Flow Including the Effects of Mass Bleed written by William Russell Seebaugh and published by . This book was released on 1968 with total page 406 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction

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ISBN 13 :
Total Pages : 916 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction by : Chen-Chih Sun

Download or read book An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction written by Chen-Chih Sun and published by . This book was released on 1977 with total page 916 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theoretical Investigation of 3-D Shock Wave-Turbulent Boundary Layer Interactions

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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Theoretical Investigation of 3-D Shock Wave-Turbulent Boundary Layer Interactions by : Doyle D. Knight

Download or read book Theoretical Investigation of 3-D Shock Wave-Turbulent Boundary Layer Interactions written by Doyle D. Knight and published by . This book was released on 1988 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: The research concerns the understanding of 3-D shock wave-turbulent boundary layer interactions. The research activity has focused on several areas. First, the 3-D swept compression corner has been computed at Mach 3 for a sweep angle of 40 deg and compression angle of 24 deg. The calculated flows are in good agreement with experiment. Second, the flowfield structure of the 3-D swept compression corner is dominated by a large vortical structure. Third, the interaction has been found quantitatively to be dominated by inviscid effects except within a small fraction of the boundary layer. Fourth, the effect of boundary layer bleed has been examined for the 3-D shock wave-turbulent boundary layer interaction generated by a sharp fin. The effects of bleed are principally limited to the near surface region. The overall vortical structure is insensitive to surface bleed. Keywords: High speed flows; Viscous-inviscid interactions; Computational fluid dynamics; Navier-Stokes equations.

An Investigation of Oblique Shock/Boundary Layer Interaction Control

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ISBN 13 :
Total Pages : 15 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis An Investigation of Oblique Shock/Boundary Layer Interaction Control by :

Download or read book An Investigation of Oblique Shock/Boundary Layer Interaction Control written by and published by . This book was released on 1993 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this work is to provide a basic understanding of the flow in the shock boundary layer interactions and of the mechanisms of their control. A parametric investigation was conducted to determine the effect of bleed configuration on the flow in the interaction region of an incident oblique shock with a turbulent boundary layer. Results of the numerical flow simulations were obtained for different slot widths, depths and slat angles over a bleed mass flow range between zero and choked conditions. The bleed results reveal a complex structure of compression expansion wave system over the bleed port entrance, and different levels of flow operation inside the slot. Code development for the implicit numerical solution of the two dimensional compressible Navier-Stokes and K- Epsilon equations was completed. The code was used in the simulation of unsteady supersonic cavity flow and the results compared with experimental data ... Shock boundary layer bleed interactions.

Preliminary Investigation of the Interaction of an Oblique Shock Wave and a Turbulent Boundary Layer

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Publisher :
ISBN 13 :
Total Pages : 200 pages
Book Rating : 4.:/5 (333 download)

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Book Synopsis Preliminary Investigation of the Interaction of an Oblique Shock Wave and a Turbulent Boundary Layer by : James Kenneth Cole

Download or read book Preliminary Investigation of the Interaction of an Oblique Shock Wave and a Turbulent Boundary Layer written by James Kenneth Cole and published by . This book was released on 1961 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of the Shock Wave-turbulent Boundary Layer Interaction

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Publisher :
ISBN 13 :
Total Pages : 544 pages
Book Rating : 4.:/5 (15 download)

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Book Synopsis An Experimental Investigation of the Shock Wave-turbulent Boundary Layer Interaction by : David William Kuntz

Download or read book An Experimental Investigation of the Shock Wave-turbulent Boundary Layer Interaction written by David William Kuntz and published by . This book was released on 1985 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theoretical Investigation of 3-D Shock Wave-Turbulent Boundary Layer Interactions

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Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Theoretical Investigation of 3-D Shock Wave-Turbulent Boundary Layer Interactions by : Doyle Knight

Download or read book Theoretical Investigation of 3-D Shock Wave-Turbulent Boundary Layer Interactions written by Doyle Knight and published by . This book was released on 1988 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research describes continuing efforts in the analysis of 3-D shock wave turbulent boundary layer interactions. A significant research activity in 3-D hypersonic shock turbulent interactions is initiated to further develop and validate the theoretical model. The quasiconical free interaction principle is examined by simulation of two geometries -17.5 deg sharp fin and (30,60) swept compression corner (Mach 3) - selected to obtain similar shock strengths. The comparison with experimental data is good. It is confirmed that the differences caused by the particular geometry of the model appear only behind the inviscid shock wave. Continuing research on 3-D turbulent interaction control is focused on the effect of bleed and the simulation of flows past the double-fin configuration. The effect of suction is examined on a strong (fin angle=20 deg, Mach 3) and a weak interaction (8 deg, Mach 3). The overall effect of bleed is remarkably modest. Two double-fin configurations (4 x 4 and 8 x 8, Mach 3) are simulated. A study of the computed flowfield indicates that the first is a weak interaction. In contrast, the 8 x 8 configuration displays an interesting separated flowfield. An analysis of viscous and inviscid effects in a sharp fin and a swept corner flow indicates that the physics of both geometries are governed primarily by inviscid (pressure) effects. Viscous effects are of lower magnitude but are not restricted to the sublayer region. High speed flows; Viscous inviscid interactions; Boundary layer interactions; Computational fluid dynamics; Navier stokes equations; Turbulence.(mjm).