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| Author | : Deepak Om |
| Publisher | : |
| Total Pages | : 358 |
| Release | : 1982 |
| Genre | : Mach number |
| 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 | : G. R. Inger |
| Publisher | : |
| Total Pages | : 8 |
| Release | : 1981 |
| Genre | : |
| ISBN | : |
Transonic normal shock - turbulent boundary layer interactions can significantly influence not only the local viscous flow but also the downstream behavior of the boundary layer on aerodynamic bodies. It is therefore important that fundamentally-based analytical tools be developed for describing and scaling these interaction effects. This paper examines recent progress toward this goal, with emphasis on two aspects. (1) A basic non-asymptotic triple-deck theory of non-separating two-dimensional interactions that is applicable over a wide range of practical Reynolds numbers and boundary layer profile shapes. (2) Its applicable as a local 'interactive module' in the global transonic flow field analysis of wings, including detailed comparisons with experimental data. Also discussed is the adaptability of this theory to treat interactions involving non-adiabatic wall conditions, including the prediction of incipient separation.
| Author | : |
| Publisher | : |
| Total Pages | : 144 |
| Release | : 1980 |
| Genre | : |
| ISBN | : |
| Author | : S.-W. Kim |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1989 |
| Genre | : |
| ISBN | : |
| Author | : George G. Mateer |
| Publisher | : |
| Total Pages | : 14 |
| Release | : 1976 |
| Genre | : |
| ISBN | : |
| Author | : M. S. Liou |
| Publisher | : |
| Total Pages | : 180 |
| Release | : 1977 |
| Genre | : |
| ISBN | : |
| Author | : W. H. Mason |
| Publisher | : |
| Total Pages | : 275 |
| Release | : 1974 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
Advances in inviscid transonic flow field computational capability and supercritical airfoil design make it important to understand of the the physics of normal shock-boundary layer interactions. In this work, the Navier-Stokes equations are thoroughly investigated through the use of perturbation methods and a generalized multi-region model is proposed for interactions between weak normal shock waves and turbulent boundary layers. This model is first applied to a highly idealized case in which a uniform subsonic flow is used to model the boundary layer, and analytic results for the wall and interface pressure are obtained.
| Author | : G. R. Inger |
| Publisher | : |
| Total Pages | : |
| Release | : 1974 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
A review is made of the existing knowledge about the interaction of impinging shock waves with laminar or turbulent boundary layers, to emphasize and illustrate that the relative degree of inviscid-dominated (solid wall-like) reflection behavior versus viscous-dominated (free surface-like) reflection is a major feature determining the disturbance flow pattern. This idea is then used to appraise existing transonic normal shock-boundary layer interaction experiments and establish an ordered relationship between them. As a result, it is shown that far from being unusual, a post-shock pocket of supersonic flow ("supersonic tongue") is in fact a common feature of all such interaction patterns, although its scale can change drastically with incident shock strength, Reynolds number and downstream conditions.
| Author | : M. S. Liou |
| Publisher | : |
| Total Pages | : |
| Release | : 1979 |
| Genre | : |
| ISBN | : |
