Experimental Investigation Of Vortex Shedding Of A Jet In Crossflow
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Experimental Investigation Of Vortex Shedding Of A Jet In Crossflow
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Author : B. Kiel
language : en
Publisher:
Release Date : 2003
Experimental Investigation Of Vortex Shedding Of A Jet In Crossflow written by B. Kiel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003 with categories.
An Experimental Investigation Of The Vortices And The Wake Associatied With A Jet In Crossflow
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Author : Dharmanshu Laxmilal Antani
language : en
Publisher:
Release Date : 1977
An Experimental Investigation Of The Vortices And The Wake Associatied With A Jet In Crossflow written by Dharmanshu Laxmilal Antani and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Jets categories.
Induces Velocity Field Of A Jet In A Crossflow
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Author : Richard L. Fearn
language : en
Publisher:
Release Date : 1978
Induces Velocity Field Of A Jet In A Crossflow written by Richard L. Fearn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Jets categories.
An experimental investigation of a subsonic round jet exhausting perpendicularly from a flat plate into a subsonic crosswind of the same temperature was conducted. Velocity and pressure measurements were made in planes perpendicular to the path of the jet for ratios of jet velocity to crossflow velocity ranging from 3 to 10. The results of these measurements are presented in tabular and graphical forms. A pair of diffuse contrarotating vortices is identified as a significant feature of the flow, and the characteristics of the vortices are discussed.
An Experimental Investigation Of Vortex Pairing In A Circular Jet Under Controlled Excitation
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Author : Khairul B. M. Quamruzzaman
language : en
Publisher:
Release Date : 1985
An Experimental Investigation Of Vortex Pairing In A Circular Jet Under Controlled Excitation written by Khairul B. M. Quamruzzaman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with Jets categories.
An Experimental Investigation Into The Effects Of Turbulence On Vortex Shedding
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Author : Richard W. Nanes
language : en
Publisher:
Release Date : 1967
An Experimental Investigation Into The Effects Of Turbulence On Vortex Shedding written by Richard W. Nanes and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.
An Experimental Investigation Of A Turbulent Jet In A Cross Flow
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Author :
language : en
Publisher:
Release Date : 1974
An Experimental Investigation Of A Turbulent Jet In A Cross Flow written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Jets categories.
Experimental Investigation Of Vortex Shedding In High Reynolds Number Flow Over Compressor Blades In Cascade
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Author : Choon P. Lim
language : en
Publisher:
Release Date : 2003-03
Experimental Investigation Of Vortex Shedding In High Reynolds Number Flow Over Compressor Blades In Cascade written by Choon P. Lim and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003-03 with categories.
An investigation of vortex shedding downstream of a cascade of compressor stator blades, at off-design inlet-flow angles of 35, 33 and 31 degrees and Reynolds numbers, based on chord length, of 625,000, 750,000 and 800,000 is reported. The objective of the study was to characterize the flow and vortex shedding through blade surface pressure measurements and hot-wire anemometry. Vortex shedding was determined to be a leading edge phenomenon as periodic shedding was only detected on the pressure side of the wake, The relationship between vortex shedding frequency and Reynolds number was nearly linear. The vortex shedding frequency at three incidence angles was observed to be quite similar at lower Reynolds number (i.e. 450,000 and below) but developed into a larger scatter at higher Reynolds number. Similarly, the Strouhal numbers were observed to be fairly consistent (0.22 to 0.24) at low Reynolds number and more scattered (0.18 to 0.25) with increasing Reynolds number. The result obtained was comparable to the experimental results obtained by Roshko Ref. 14, for vortex shedding behind a circular cylinder.
An Experimental Investigation Of A Turbulent Jet In A Cross Flow
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Author : David Kenneth Mosher
language : en
Publisher:
Release Date : 1970
An Experimental Investigation Of A Turbulent Jet In A Cross Flow written by David Kenneth Mosher and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Jets categories.
The interference phenomenon occurring when a subsonic turbulent jet exhausts normally from a large flat plate into a low speed crossflow was experimentally investigated in the Georgia Tech nine foot wind tunnel. Static pressures were measured on the surface around the jet. In the region off the surface, including the jet plume, wake and surrounding areas, the average total and static pressures and the average velocity magnitudes and directions were determined. Three jet exit configurations were studied, one circular and two slot-shaped with width to length ratios of 0.3 and 3.4. All have the same exit area. The effective jet to cross-flow velocity ratio was varied, for each of the exit configurations, over the range 4.0 to 12.0. Analysis of the data indicates that the pressure distributions induced on the surface are a combined result of the jet's blocking and entraining effects on the cross flow with entrainment becoming the more dominant of the two as the effective velocity ratio is increased. This relative dominance brings about an attenuation of total interference lift loss (when computed as a fraction of gross thrust) primarily by causing a rise in the low pressures in the wake region as the effective velocity ratio increases. When the effective velocity ratio is held fixed, the total interference lift loss increases with increasing width to length ratio of the jet exit. (Author).
Experimental And Numerical Investigation Of Vortex Shedding
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Author : Abubaker Awidat Salem
language : en
Publisher:
Release Date : 1998
Experimental And Numerical Investigation Of Vortex Shedding written by Abubaker Awidat Salem and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
Experimental Investigation Of Radial Inflow Vortexes In Jet Injection And Rotating Peripheral Wall Water Vortex Tubes
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Author : Arthur Travers
language : en
Publisher:
Release Date : 1968
Experimental Investigation Of Radial Inflow Vortexes In Jet Injection And Rotating Peripheral Wall Water Vortex Tubes written by Arthur Travers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Injections categories.
