Author: C.C. HorstmanPublisher:
ISBN:
Category :
Languages : en
Pages : 10
Book Description
Prediction of Hypersonic Shock-wave/turbulent-boundary-layer Interaction Flows
Author: C.C. HorstmanDocumentation of Two- and Three-dimensional Hypersonic Shock Wave/turbulent Boundary Layer Interaction Flows
Author: Marvin I. KussoyPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 32
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger BabinskyPublisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
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.
Prediction of Hypersonic Shock Wave Turbulent Boundary Layer Interactions with the K-l Two-equation Turbulence Model
Author: Brian R. SmithHypersonic Shock-wave Turbulent Boundary Layer Interaction Flows
Author: C. C. HorstmannAn Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation
Author: Documentation of Two- And Three-Dimensional Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722182298
Category :
Languages : en
Pages : 28
Book Description
Experimental data for a series of two- and three-dimensional shock wave/turbulent boundary layer interaction flows at Mach 7 are presented. Test bodies, composed of simple geometric shapes, were designed to generate flows with varying degrees of pressure gradient, boundary-layer separation, and turning angle. The data include surface-pressure and heat-transfer distributions as well as limited mean-flow-field surveys in both the undisturbed and the interaction regimes. The data are presented in a convenient form for use in validating existing or future computational models of these generic hypersonic flows. Kussoy, Marvin I. and Horstman, Clifford C. Ames Research Center NCC2-452; RTOP 505-80-11...
Understanding and Predicting Shockwave and Turbulent Boundary Layer Interactions
Author: M. Pino MartinPublisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 34
Book Description
Shockwave and turbulent boundary layer interactions produce intense localized pressure loads and heating rates that can have a dramatic influence on the drag and heating experienced by a high-speed vehicle, and can significantly impact fuel mixing and combustion in propulsion systems. The lack of standardized and traceable databases prevents the calibration of computational fluid dynamic models to accurately represent these critical flow phenomena. In this work we accomplished the development and validation against experiments at the same flow and boundary conditions of direct numerical simulations of shock and turbulent boundary layer interactions. We pioneered the development of a unique numerical capability that allows the accurate and detailed three-dimensional turbulence data at a reasonable turn-around time. In turn, parametric studies of fundamental flow physics are feasible, for the first time. By accurate, it is meant that the numerical uncertainty is within the experimental error.
Shock Wave - Turbulent Boundary Layer Interaction in Hypersonic Flow
Author: M. S. HoldenPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
Book Description
Shock Wave - Turbulent Boundary Layer Interaction in Hypersonic Flow
Author: Michael S. HoldenPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 69
Book Description