Author: Ralph D. Cooper
Publisher:
ISBN:
Category : Cavitation
Languages : en
Pages : 602
Book Description
Hydrodynamic Noise, Cavity Flow
Author: Ralph D. Cooper
Publisher:
ISBN:
Category : Cavitation
Languages : en
Pages : 602
Book Description
Publisher:
ISBN:
Category : Cavitation
Languages : en
Pages : 602
Book Description
Mach 0.6 to 3.0 Flows Over Rectangular Cavities
Author: Louis G. Kaufman
Publisher:
ISBN:
Category : Aeroacoustics
Languages : en
Pages : 288
Book Description
Internal weapons carriage in high performance aircraft is often adversely affected by the severe aeroacoustic environment produced with the weapons bay doors open. To obtain a better understanding of this fluid dynamic problem, basic static and oscillatory pressure data were obtained for Mach 0.6 to 3.0 flows over shallow rectangular cavities in a generic flat plate model. Cavity length to depth ratios were varied from approximately 5 to 10. Static pressure data characteristic of both open and closed cavity flows were obtained. An improved Rossiter method is presented that satisfactorily predicts the possible frequency modes within the cavity. Highest fluctuating pressure occurs on the aft bulkhead, peaking near Mach 1.5 for the conditions tested. Aeroacoustic levels are substantially reduced by installing suppression fences (spoilers) at subsonic and low supersonic conditions. Acoustic levels generally drop rapidly above Mach 1.5. (Author).
Publisher:
ISBN:
Category : Aeroacoustics
Languages : en
Pages : 288
Book Description
Internal weapons carriage in high performance aircraft is often adversely affected by the severe aeroacoustic environment produced with the weapons bay doors open. To obtain a better understanding of this fluid dynamic problem, basic static and oscillatory pressure data were obtained for Mach 0.6 to 3.0 flows over shallow rectangular cavities in a generic flat plate model. Cavity length to depth ratios were varied from approximately 5 to 10. Static pressure data characteristic of both open and closed cavity flows were obtained. An improved Rossiter method is presented that satisfactorily predicts the possible frequency modes within the cavity. Highest fluctuating pressure occurs on the aft bulkhead, peaking near Mach 1.5 for the conditions tested. Aeroacoustic levels are substantially reduced by installing suppression fences (spoilers) at subsonic and low supersonic conditions. Acoustic levels generally drop rapidly above Mach 1.5. (Author).
Cavity Unsteady-Pressure Measurements at Subsonic and Transonic Speeds
Author: Maureen B. Tracy
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 84
Book Description
Cellular Flows
Author: Vladimir Shtern
Publisher: Cambridge University Press
ISBN: 1108311210
Category : Technology & Engineering
Languages : en
Pages : 589
Book Description
A cell, whose spatial extent is small compared with a surrounding flow, can develop inside a vortex. Such cells, often referred to as vortex breakdown bubbles, provide stable and clean flame in combustion chambers; they also reduce the lift force of delta wings. This book analyzes cells in slow and fast, one- and two-fluid flows and describes the mechanisms of cell generation: (a) minimal energy dissipation, (b) competing forces, (c) jet entrainment, and (d) swirl decay. The book explains the vortex breakdown appearance, discusses its features, and indicates means of its control. Written in acceptable, non-math-heavy format, it stands to be a useful learning tool for engineers working with combustion chambers, chemical and biological reactors, and delta-wing designs.
Publisher: Cambridge University Press
ISBN: 1108311210
Category : Technology & Engineering
Languages : en
Pages : 589
Book Description
A cell, whose spatial extent is small compared with a surrounding flow, can develop inside a vortex. Such cells, often referred to as vortex breakdown bubbles, provide stable and clean flame in combustion chambers; they also reduce the lift force of delta wings. This book analyzes cells in slow and fast, one- and two-fluid flows and describes the mechanisms of cell generation: (a) minimal energy dissipation, (b) competing forces, (c) jet entrainment, and (d) swirl decay. The book explains the vortex breakdown appearance, discusses its features, and indicates means of its control. Written in acceptable, non-math-heavy format, it stands to be a useful learning tool for engineers working with combustion chambers, chemical and biological reactors, and delta-wing designs.
Characterization of Cavity Flow Fields Using Pressure Data Obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author: Maureen B. Tracy
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 40
Book Description
The Theory of Subsonic Plane Flow
Vortex Flows at Supersonic Speeds
Author: Richard M. Wood
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 104
Book Description
Computational Modelling of Bifurcations and Instabilities in Fluid Dynamics
Author: Alexander Gelfgat
Publisher: Springer
ISBN: 3319914944
Category : Technology & Engineering
Languages : en
Pages : 524
Book Description
Instabilities of fluid flows and the associated transitions between different possible flow states provide a fascinating set of problems that have attracted researchers for over a hundred years. This book addresses state-of-the-art developments in numerical techniques for computational modelling of fluid instabilities and related bifurcation structures, as well as providing comprehensive reviews of recently solved challenging problems in the field.
Publisher: Springer
ISBN: 3319914944
Category : Technology & Engineering
Languages : en
Pages : 524
Book Description
Instabilities of fluid flows and the associated transitions between different possible flow states provide a fascinating set of problems that have attracted researchers for over a hundred years. This book addresses state-of-the-art developments in numerical techniques for computational modelling of fluid instabilities and related bifurcation structures, as well as providing comprehensive reviews of recently solved challenging problems in the field.
Food Engineering in a Computer Climate
Author:
Publisher: CRC Press
ISBN: 9781560322559
Category : Business & Economics
Languages : en
Pages : 556
Book Description
Based on papers presented at a conference on food engineering, this book addresses the whole food production process, from receiving the raw materials through to packaging and distribution. Major themes are the opportunities/limitations afforded by the application of modern computer technology.
Publisher: CRC Press
ISBN: 9781560322559
Category : Business & Economics
Languages : en
Pages : 556
Book Description
Based on papers presented at a conference on food engineering, this book addresses the whole food production process, from receiving the raw materials through to packaging and distribution. Major themes are the opportunities/limitations afforded by the application of modern computer technology.
Computational Fluid Dynamics 2000
Author: Nobuyuki Satofuka
Publisher: Springer Science & Business Media
ISBN: 3642565352
Category : Science
Languages : en
Pages : 807
Book Description
These proceedings contain a selection of refereed contributions as a source of reference for all those interested in the state of the art in computational fluid dynamics. The conference brings together physicists, mathematicians and engineers to review and share recent advances in the field.
Publisher: Springer Science & Business Media
ISBN: 3642565352
Category : Science
Languages : en
Pages : 807
Book Description
These proceedings contain a selection of refereed contributions as a source of reference for all those interested in the state of the art in computational fluid dynamics. The conference brings together physicists, mathematicians and engineers to review and share recent advances in the field.