Numerical Simulation of a Confined Transonic Normal Shock Wave/turbulent Boundary Layer Interaction PDF Download
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Author: E. Blosch
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: E. Blosch
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
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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.
Author: David Nixon
Publisher:
ISBN:
Category :
Languages : en
Pages : 94
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This report describes the results of research into the interactions between shock waves and turbulent flows using numerical simulations. The research was conducted at transonic speeds with a normal shock wave and two dimensional turbulence, making use of existing knowledge and computational methods for developing insight to the shock/turbulence interaction. The results indicate that the shock has a significant effect on the turbulence. The shock produces a jump in the turbulence statistics, with a long relaxation distance to return to unshocked values. The turbulence kinetic energy is increased by as much as 30 percent by the shock. The density-velocity correlation becomes important during the shock jump and is greatly increased over the case without a shock. On the other hand, the pressure-velocity correlation is not so important. The shock speed and ripple were found to be important factors in determining the turbulence downstream of a shock wave. Shock speed and ripple correlations are the same size as other important turbulence correlations. The work must be extended to higher Mach numbers and three-dimensional turbulence, with oblique shocks and shear flows. The shock ripple may be more important for oblique shocks because of the larger v component. (jhd).
Author: Thomas Charles Adamson
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 152
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Author: Thomas A. Zang
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 40
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 144
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Author: Wei-Li Yang
Publisher:
ISBN:
Category :
Languages : en
Pages : 398
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Author: S.-W. Kim
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
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Author: Marianna Gnedin
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
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Author: Deepak Om
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 358
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