A Numerical Solution for the Interaction of a Moving Shock Wave with a Turbulent Mixing Region
Author | : William Fred Walker |
Publisher | : |
Total Pages | : 216 |
Release | : 1966 |
Genre | : Shock waves |
ISBN | : |
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Author | : William Fred Walker |
Publisher | : |
Total Pages | : 216 |
Release | : 1966 |
Genre | : Shock waves |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 884 |
Release | : 1968 |
Genre | : Mechanical engineering |
ISBN | : |
Publishes original research in all branches of mechanics including aerodynamics; aeroelasticity; boundary layers; computational mechanics; constitutive modeling of materials; dynamics; elasticity; flow and fracture; heat transfer; hydraulics; impact; internal flow; mechanical properties of materials; micromechanics; plasticity; stress analysis; structures; thermodynamics; turbulence; vibration; and wave propagation.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 1000 |
Release | : 1971 |
Genre | : Aeronautics |
ISBN | : |
Author | : Thomas Charles Adamson |
Publisher | : |
Total Pages | : 152 |
Release | : 1980 |
Genre | : Shock waves |
ISBN | : |
Author | : Holger Babinsky |
Publisher | : Cambridge University Press |
Total Pages | : 481 |
Release | : 2011-09-12 |
Genre | : Technology & Engineering |
ISBN | : 1139498649 |
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.
Author | : Piotr Doerffer |
Publisher | : Springer Nature |
Total Pages | : 540 |
Release | : 2020-07-30 |
Genre | : Technology & Engineering |
ISBN | : 3030474615 |
This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.
Author | : Sanida Laboratories. Simulated Environments Information Center |
Publisher | : |
Total Pages | : 40 |
Release | : 1968 |
Genre | : Buildings |
ISBN | : |
Author | : Seán Prunty |
Publisher | : Springer Nature |
Total Pages | : 356 |
Release | : 2021-01-22 |
Genre | : Science |
ISBN | : 3030636062 |
This book provides an elementary introduction to one-dimensional fluid flow problems involving shock waves in air. The differential equations of fluid flow are approximated by finite difference equations and these in turn are numerically integrated in a stepwise manner, with artificial viscosity introduced into the numerical calculations in order to deal with shocks. This treatment of the subject is focused on the finite-difference approach to solve the coupled differential equations of fluid flow and presents the results arising from the numerical solution using Mathcad programming. Both plane and spherical shock waves are discussed with particular emphasis on very strong explosive shocks in air. This expanded second edition features substantial new material on sound wave parameters, Riemann's method for numerical integration of the equations of motion, approximate analytical expressions for weak shock waves, short duration piston motion, numerical results for shock wave interactions, and new appendices on the piston withdrawal problem and numerical results for a closed shock tube. This text will appeal to students, researchers, and professionals in shock wave research and related fields. Students in particular will appreciate the benefits of numerical methods in fluid mechanics and the level of presentation.