Asymptotic Structure of Supersonic Turbulent Boundary Layers

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ISBN 13 :
Total Pages : 552 pages
Book Rating : 4.:/5 (39 download)

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Book Synopsis Asymptotic Structure of Supersonic Turbulent Boundary Layers by : Jun He

Download or read book Asymptotic Structure of Supersonic Turbulent Boundary Layers written by Jun He and published by . This book was released on 1993 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:

(U) Physical Models for Supersonic Turbulent Boundary Layer Structure

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis (U) Physical Models for Supersonic Turbulent Boundary Layer Structure by : Alexander J. Smits

Download or read book (U) Physical Models for Supersonic Turbulent Boundary Layer Structure written by Alexander J. Smits and published by . This book was released on 1989 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

ASYMPTOTIC THEORY OF AN UNSEPARATED SUPERSONIC TURBULENT BOUNDARY LAYER AT A COMPRESSION CORNER.

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ISBN 13 :
Total Pages : 187 pages
Book Rating : 4.:/5 (682 download)

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Book Synopsis ASYMPTOTIC THEORY OF AN UNSEPARATED SUPERSONIC TURBULENT BOUNDARY LAYER AT A COMPRESSION CORNER. by : SHREEKANT AGRAWAL

Download or read book ASYMPTOTIC THEORY OF AN UNSEPARATED SUPERSONIC TURBULENT BOUNDARY LAYER AT A COMPRESSION CORNER. written by SHREEKANT AGRAWAL and published by . This book was released on 1983 with total page 187 pages. Available in PDF, EPUB and Kindle. Book excerpt: transverse length scale equal to the boundary-layer thickness, inviscid-flow solutions are derived in a supersonic, a hypersonic, and a transonic small-disturbance limit. Additional intermediate inviscid-flow solutions are derived in supersonic and transonic limits in order to describe the flow field at smaller distances from the corner.

Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers by : Alexander J. Smits

Download or read book Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers written by Alexander J. Smits and published by . This book was released on 1988 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Supersonic Boundary Layer Transition and Turbulent Structure

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation of Supersonic Boundary Layer Transition and Turbulent Structure by : Alexander J. Smits

Download or read book Investigation of Supersonic Boundary Layer Transition and Turbulent Structure written by Alexander J. Smits and published by . This book was released on 1990 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Structure of Supersonic Turbulent Boundary Layers Subjected to Concave Surface Curvature

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ISBN 13 :
Total Pages : 652 pages
Book Rating : 4.:/5 (223 download)

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Book Synopsis The Structure of Supersonic Turbulent Boundary Layers Subjected to Concave Surface Curvature by : John Francis Donovan

Download or read book The Structure of Supersonic Turbulent Boundary Layers Subjected to Concave Surface Curvature written by John Francis Donovan and published by . This book was released on 1989 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis of the Three-dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow

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ISBN 13 :
Total Pages : 98 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Analysis of the Three-dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow by : John C. Adams

Download or read book Analysis of the Three-dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow written by John C. Adams and published by . This book was released on 1972 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.

Organized Structures in a Supersonic Turbulent Boundary Layer

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ISBN 13 :
Total Pages : 466 pages
Book Rating : 4.:/5 (86 download)

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Book Synopsis Organized Structures in a Supersonic Turbulent Boundary Layer by : Eric Francis Spina

Download or read book Organized Structures in a Supersonic Turbulent Boundary Layer written by Eric Francis Spina and published by . This book was released on 1988 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Organized Structures in a Supersonic Turbulent Boundary Layer

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ISBN 13 :
Total Pages : 466 pages
Book Rating : 4.:/5 (86 download)

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Book Synopsis Organized Structures in a Supersonic Turbulent Boundary Layer by : Eric Francis Spina

Download or read book Organized Structures in a Supersonic Turbulent Boundary Layer written by Eric Francis Spina and published by . This book was released on 1988 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722453923
Total Pages : 44 pages
Book Rating : 4.4/5 (539 download)

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Book Synopsis On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure by : National Aeronautics and Space Administration (NASA)

Download or read book On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-09 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A mathematical model and a computer code have been developed to fully couple the vibration of an aircraft fuselage panel to the surrounding flow field, turbulent boundary layer and acoustic fluid. The turbulent boundary layer model is derived using a triple decomposition of the flow variables and applying a conditional averaging to the resulting equations. Linearized panel and acoustic equations are used. Results from this model are in good agreement with existing experimental and numerical data. It is shown that in the supersonic regime, full coupling of the flexible panel leads to lower response and radiation from the panel. This is believed to be due to an increase in acoustic damping on the panel in this regime. Increasing the Mach number increases the acoustic damping, which is in agreement with earlier work. Frendi, Abdelkader Unspecified Center NAS1-19700; RTOP 537-06-37-20...

On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure by : Abdelkader Frendi

Download or read book On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure written by Abdelkader Frendi and published by . This book was released on 1996 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Turbulent Shear Layers in Supersonic Flow

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Publisher : Springer Science & Business Media
ISBN 13 : 0387263055
Total Pages : 418 pages
Book Rating : 4.3/5 (872 download)

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Book Synopsis Turbulent Shear Layers in Supersonic Flow by : Alexander J. Smits

Download or read book Turbulent Shear Layers in Supersonic Flow written by Alexander J. Smits and published by Springer Science & Business Media. This book was released on 2006-05-11 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt: A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.

The Response of a Laminar Boundary Layer in Supersonic Flow to Small Amplitude Progressive Waves

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722881436
Total Pages : 40 pages
Book Rating : 4.8/5 (814 download)

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Book Synopsis The Response of a Laminar Boundary Layer in Supersonic Flow to Small Amplitude Progressive Waves by : National Aeronautics and Space Administration (NASA)

Download or read book The Response of a Laminar Boundary Layer in Supersonic Flow to Small Amplitude Progressive Waves written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-13 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effect of a small amplitude progressive wave on the laminar boundary layer on a semi-infinite flat plate, due to a uniform supersonic freestream flow, is considered. The perturbation to the flow divides into two streamwise zones. In the first, relatively close to the leading edge of the plate, on a transverse scale comparable to the boundary layer thickness, the perturbation flow is described by a form of the unsteady linearized compressible boundary layer equations. In the freestream, this component of flow is governed by the wave equation, the solution of which provides the outer velocity conditions for the boundary layer. This system is solved numerically, and also the asymptotic structure in the far downstream limit is studied. This reveals a breakdown and a subsequent second streamwise zone, where the flow disturbance is predominantly inviscid. The two zones are shown to match in a proper asymptotic sense. Duck, Peter W. Glenn Research Center NASA ORDER C-99066-G; RTOP 505-62-27...

Fundamental Aspects of the Structure of Supersonic Turbulent Boundary

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ISBN 13 :
Total Pages : 41 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Fundamental Aspects of the Structure of Supersonic Turbulent Boundary by : Jonathan H. Watmuff

Download or read book Fundamental Aspects of the Structure of Supersonic Turbulent Boundary written by Jonathan H. Watmuff and published by . This book was released on 1987 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of structure angle in a supersonic turbulent boundary layer with zero and adverse pressure gradients are presented. Conditionally sampled measurements of u, v, and uv are presented along with quadrant analysis of the turbulent fluctuations. The latter suggests ambiguities associated with the interpretation of VITA measurements. Preliminary results of experiments on artificially generated hairpin vortices are also discussed. Measurements indicate a high degree of similarity between the signatures of these hairpin structures and ensemble averaged events in the turbulent boundary layer. Keywords: Turbulence, Boundary layer, Supersonic Flow.

Structure of the supersonic turbulent boundary layer and its influence on unsteady separation

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ISBN 13 :
Total Pages : 510 pages
Book Rating : 4.:/5 (349 download)

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Book Synopsis Structure of the supersonic turbulent boundary layer and its influence on unsteady separation by : Ömer Haldun Ünalmiş

Download or read book Structure of the supersonic turbulent boundary layer and its influence on unsteady separation written by Ömer Haldun Ünalmiş and published by . This book was released on 1995 with total page 510 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Physical Models for Supersonic Turbulent Boundary Layer Structure

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Physical Models for Supersonic Turbulent Boundary Layer Structure by :

Download or read book Physical Models for Supersonic Turbulent Boundary Layer Structure written by and published by . This book was released on 1989 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental program was carried out to study the detailed structure of supersonic turbulent boundary layers. The experiments were designed to elucidate physical models and mechanisms that are particular to compressible turbulence, such as the effects of compressibility on the nature of the large- scale motions, the scaling laws for high Reynolds number supersonic turbulent flows, direct compressibility effects that cause the exchange of turbulence energy among the vorticity, entropy and sound modes, and the transport of heat and momentum by compressible turbulent motions. A description of the new optical experimental tools that were developed is included. (EDC).

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 380 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.