A Numerical Investigation of Supersonic Turbulent Shear Layers - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook A Numerical Investigation of Supersonic Turbulent Shear Layers write by Choong K. Oh. This book was released on 1994. A Numerical Investigation of Supersonic Turbulent Shear Layers available in PDF, EPUB and Kindle.
Turbulent Shear Layers in Supersonic Flow
Turbulent Shear Layers in Supersonic Flow - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Turbulent Shear Layers in Supersonic Flow write by Alexander J. Smits. This book was released on 2006-05-11. Turbulent Shear Layers in Supersonic Flow available in PDF, EPUB and Kindle. 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.
Numerical Investigation of Supersonic Turbulent Boundary Layers
Numerical Investigation of Supersonic Turbulent Boundary Layers - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Numerical Investigation of Supersonic Turbulent Boundary Layers write by Thierry Maeder. This book was released on 2000. Numerical Investigation of Supersonic Turbulent Boundary Layers available in PDF, EPUB and Kindle.
An Experimental Investigation of Scalar Mixing in Supersonic Turbulent Shear Layers
An Experimental Investigation of Scalar Mixing in Supersonic Turbulent Shear Layers - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook An Experimental Investigation of Scalar Mixing in Supersonic Turbulent Shear Layers write by Noel T. Clemens. This book was released on 1991. An Experimental Investigation of Scalar Mixing in Supersonic Turbulent Shear Layers available in PDF, EPUB and Kindle.
Numerical Investigation of Compressible Turbulent Boundary Layers
Numerical Investigation of Compressible Turbulent Boundary Layers - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Numerical Investigation of Compressible Turbulent Boundary Layers write by Muhammad Farrukh Shahab. This book was released on 2012-02. Numerical Investigation of Compressible Turbulent Boundary Layers available in PDF, EPUB and Kindle. As a prerequisite for relevant model development and improvement of design methodologies for supersonic vehicles, this study aims at investigating the influence of wall heat-transfer and shock interaction on the turbulence structure of supersonic boundary layers. Incipient separation conditions and two different wall thermal boundary conditions (adiabatic and cold) are considered. The analysis focuses on the evolution of mean and turbulent flow properties along the interaction region and in the relaxation region downstream of the shock-system. The strong influence of the mean pressure gradient is quantified through the analysis of mean flow profiles and boundary layer integral parameters. The anisotropic amplification of turbulent quantities through the interaction region is characterized and the turbulent events associated with the modification of the turbulence structure of the perturbed boundary layer are identified. The mean and turbulent thermal fields are shown to be strongly modified by the wall cooling which significantly dampens more particularly the turbulent thermal quantities levels across the boundary layer.
