Direct Numerical Simulation of Acoustic Waves Interacting with a Shock Wave in a Quasi-1D Convergent-divergent Nozzle Using an Unstructured Finite Volume Algorithm PDF Download
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Languages : en
Pages : 10
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Languages : en
Pages : 10
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Author: Trong T. Bui
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Category : Parallel computers
Languages : en
Pages : 28
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Category : Aeronautics
Languages : en
Pages : 940
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Category : Government publications
Languages : en
Pages : 652
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Category : Mathematics
Languages : en
Pages : 184
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Languages : en
Pages : 192
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Category : Science
Languages : en
Pages : 796
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Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
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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: Xiao-Yen Wang
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Languages : en
Pages : 20
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Author: Michael F. Hess
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Languages : en
Pages : 65
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