An Experimental Study of the Interaction of a Plane Shock Wave with a Contact Region PDF Download
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Author: University of Toronto. Institute of Aerophysics
Publisher: Institute of Aerophysics, University of Toronto
ISBN:
Category : Gas flow
Languages : en
Pages : 47
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Book Description
Author: University of Toronto. Institute of Aerophysics
Publisher: Institute of Aerophysics, University of Toronto
ISBN:
Category : Gas flow
Languages : en
Pages : 47
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Book Description
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: University of Toronto. Institute of Aerophysics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 406
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 608
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Book Description
Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642
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Book Description
Author: David L. Merritt
Publisher:
ISBN:
Category : Ballistic ranges
Languages : en
Pages : 100
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Book Description
A ballistics range and a shocktube were used to study head-on interactions between 9-degree cones flying at supersonic speeds and plane shock waves. Photographs of the shock-shock interaction were taken. Experimental shock wave patterns agreed with predicted patterns. The reflected shock wave produced little or no overpressure on the model. (Author).
Author: I. I. Glass
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 88
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1142
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Book Description
Author: J.W. Allan
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
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Book Description
