Author: Richard Bivins Countess
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 128
Book Description
An Experimental Investigation of a Supersonic Gas Jet Impinging Into a Liquid
Author: Richard Bivins Countess
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 128
Book Description
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 128
Book Description
An Experimental Investigation of a Liquid Film on a Horizontal Flat Plate in a Supersonic Gas Stream
Author: Billy Wayne Marshall
Publisher:
ISBN:
Category :
Languages : en
Pages : 510
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 510
Book Description
Experimental Investigation of Supersonic Impinging Jets in Stovl Configuration
Author: Kartik G. Iyer
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 276
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 276
Book Description
Experimental Investigation of Multiple-jet Liquid Injection Into Hypersonic Flow
Author: William F. Hinson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 50
Book Description
Experimental Investigation of the Formation of a Gas Jet Behind the Front of a Shock Wave in the Outflow of Divergent and Supersonic Nozzles
Author: A. I. Starshinov
Publisher:
ISBN:
Category :
Languages : en
Pages : 8
Book Description
A shock tube was used in carrying out the investigations. Dimensions of the nozzles used in the experiment are given together with empirical formulas obtained.
Publisher:
ISBN:
Category :
Languages : en
Pages : 8
Book Description
A shock tube was used in carrying out the investigations. Dimensions of the nozzles used in the experiment are given together with empirical formulas obtained.
29th International Symposium on Shock Waves 2
Author: Riccardo Bonazza
Publisher:
ISBN: 9783319168395
Category :
Languages : en
Pages :
Book Description
This proceedings present the results of the 29th International Symposium on Shock Waves (ISSW29) which was held in Madison, Wisconsin, U.S.A., from July 14 to July 19, 2013. It was organized by the Wisconsin Shock Tube Laboratory, which is part of the College of Engineering of the University of Wisconsin-Madison. The ISSW29 focused on the following areas: Blast Waves, Chemically Reactive Flows, Detonation and Combustion, Facilities, Flow Visualization, Hypersonic Flow, Ignition, Impact and Compaction, Industrial Applications, Magnetohydrodynamics, Medical and Biological Applications, Nozzle Flow, Numerical Methods, Plasmas, Propulsion, Richtmyer-Meshkov Instability, Shock-Boundary Layer Interaction, Shock Propagation and Reflection, Shock Vortex Interaction, Shock Waves in Condensed Matter, Shock Waves in Multiphase Flow, as well as Shock Waves in Rarefield Flow. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 29 and individuals interested in these fields.
Publisher:
ISBN: 9783319168395
Category :
Languages : en
Pages :
Book Description
This proceedings present the results of the 29th International Symposium on Shock Waves (ISSW29) which was held in Madison, Wisconsin, U.S.A., from July 14 to July 19, 2013. It was organized by the Wisconsin Shock Tube Laboratory, which is part of the College of Engineering of the University of Wisconsin-Madison. The ISSW29 focused on the following areas: Blast Waves, Chemically Reactive Flows, Detonation and Combustion, Facilities, Flow Visualization, Hypersonic Flow, Ignition, Impact and Compaction, Industrial Applications, Magnetohydrodynamics, Medical and Biological Applications, Nozzle Flow, Numerical Methods, Plasmas, Propulsion, Richtmyer-Meshkov Instability, Shock-Boundary Layer Interaction, Shock Propagation and Reflection, Shock Vortex Interaction, Shock Waves in Condensed Matter, Shock Waves in Multiphase Flow, as well as Shock Waves in Rarefield Flow. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 29 and individuals interested in these fields.
Proceedings of the 8th Pacific Rim International Conference on Advanced Materials and Processing (PRICM-8)
Author: FernD.S. Marquis
Publisher: Springer
ISBN: 3319487647
Category : Technology & Engineering
Languages : en
Pages : 3431
Book Description
PRICM-8 features the most prominent and largest-scale interactions in advanced materials and processing in the Pacific Rim region. The conference is unique in its intrinsic nature and architecture which crosses many traditional discipline and cultural boundaries. This is a comprehensive collection of papers from the 15 symposia presented at this event.
Publisher: Springer
ISBN: 3319487647
Category : Technology & Engineering
Languages : en
Pages : 3431
Book Description
PRICM-8 features the most prominent and largest-scale interactions in advanced materials and processing in the Pacific Rim region. The conference is unique in its intrinsic nature and architecture which crosses many traditional discipline and cultural boundaries. This is a comprehensive collection of papers from the 15 symposia presented at this event.
Experimental Investigation of Fluid Structure Interactions in Supersonic Flows
Author: Santosh Vaibhav Varigonda
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
An Experimental Study of Two-Dimensional Supersonic Jet Impingement on a Flat Plate
Author: T. F. Zien
Publisher:
ISBN:
Category :
Languages : en
Pages : 94
Book Description
An experimental study of the flow field associated with a two-dimensional, supersonic jet impinging normally on a flat plate is reported. Two wedge nozzles manufactured at the design Mach numbers of 1.75 and 2.75, respectively, were used to provide the jet. Extensive pitot surveys of the free jet were first conducted to determine the quality of the free jet. Results indicate that the simple wedge nozzles were adequate in providing the desired two-dimensional jet in the free expansion configuration. Results of surface pressure measurements and schlieren photographs of the impingement flow indicating the shock patterns are then presented and discussed. Although the results are principally reported for the case of the jet at isentropic exit conditions, some results of underexpanded and overexpanded jets are also included. Some discrepancies between the experiment and the simple theory based in the method of integral relations and the inviscid flow model are noted and discussed. An 'effective' jet Mach number is introduced which accounts largely for the discrepancy between experiments and theory, and its determination is based on the measured stagnation point pressure on the plate surface. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 94
Book Description
An experimental study of the flow field associated with a two-dimensional, supersonic jet impinging normally on a flat plate is reported. Two wedge nozzles manufactured at the design Mach numbers of 1.75 and 2.75, respectively, were used to provide the jet. Extensive pitot surveys of the free jet were first conducted to determine the quality of the free jet. Results indicate that the simple wedge nozzles were adequate in providing the desired two-dimensional jet in the free expansion configuration. Results of surface pressure measurements and schlieren photographs of the impingement flow indicating the shock patterns are then presented and discussed. Although the results are principally reported for the case of the jet at isentropic exit conditions, some results of underexpanded and overexpanded jets are also included. Some discrepancies between the experiment and the simple theory based in the method of integral relations and the inviscid flow model are noted and discussed. An 'effective' jet Mach number is introduced which accounts largely for the discrepancy between experiments and theory, and its determination is based on the measured stagnation point pressure on the plate surface. (Author).
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description