Effect of Initial Tangential Velocity Distribution on the Mean Evolution of a Swirling Turbulent Free Jet

Effect of Initial Tangential Velocity Distribution on the Mean Evolution of a Swirling Turbulent Free Jet PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725734821
Category :
Languages : en
Pages : 26

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An existing cold jet facility at NASA-Lewis was modified to produce swirling flows with controllable initial tangential velocity distribution. Distinctly different swirl velocity profiles were produced, and their effects on jet mixing characteristics were measured downstream of an 11.43 cm diameter convergent nozzle. It was experimentally shown that in the near field of a swirling turbulent jet, the mean velocity field strongly depends on the initial swirl profile. Two extreme tangential velocity distributions were produced. The two jets shared approximately the same initial mass flow rate of 5.9 kg/s, mass averaged axial Mach number and swirl number. Mean centerline velocity decay characteristics of the solid body rotation jet flow exhibited classical decay features of a swirling jet with S = 0.48 reported in the literature. It is concluded that the integrated swirl effect, reflected in the swirl number, is inadequate in describing the mean swirling jet behavior in the near field. Farokhi, S. and Taghavi, R. and Rice, E. J. Glenn Research Center NASA-TM-100934, E-4211, NAS 1.15:100934 NCC3-56; RTOP 505-62-21...

Effect of Initial Tangential Velocity Distribution on the Mean Evolution of a Swirling Turbulent Free Jet

Effect of Initial Tangential Velocity Distribution on the Mean Evolution of a Swirling Turbulent Free Jet PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725734821
Category :
Languages : en
Pages : 26

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Book Description
An existing cold jet facility at NASA-Lewis was modified to produce swirling flows with controllable initial tangential velocity distribution. Distinctly different swirl velocity profiles were produced, and their effects on jet mixing characteristics were measured downstream of an 11.43 cm diameter convergent nozzle. It was experimentally shown that in the near field of a swirling turbulent jet, the mean velocity field strongly depends on the initial swirl profile. Two extreme tangential velocity distributions were produced. The two jets shared approximately the same initial mass flow rate of 5.9 kg/s, mass averaged axial Mach number and swirl number. Mean centerline velocity decay characteristics of the solid body rotation jet flow exhibited classical decay features of a swirling jet with S = 0.48 reported in the literature. It is concluded that the integrated swirl effect, reflected in the swirl number, is inadequate in describing the mean swirling jet behavior in the near field. Farokhi, S. and Taghavi, R. and Rice, E. J. Glenn Research Center NASA-TM-100934, E-4211, NAS 1.15:100934 NCC3-56; RTOP 505-62-21...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704

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Turbulent Swirling Jets with Excitation

Turbulent Swirling Jets with Excitation PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724700643
Category :
Languages : en
Pages : 230

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An existing cold-jet facility at NASA Lewis Research Center was modified to produce swirling flows with controllable initial tangential velocity distribution. Two extreme swirl profiles, i.e., one with solid-body rotation and the other predominated by a free-vortex distribution, were produced at identical swirl number of 0.48. Mean centerline velocity decay characteristics of the solid-body rotation jet flow exhibited classical decay features of a swirling jet with S - 0.48 reported in the literature. However, the predominantly free-vortex distribution case was on the verge of vortex breakdown, a phenomenon associated with the rotating flows of significantly higher swirl numbers, i.e., S sub crit greater than or equal to 0.06. This remarkable result leads to the conclusion that the integrated swirl effect, reflected in the swirl number, is inadequate in describing the mean swirling jet behavior in the near field. The relative size (i.e., diameter) of the vortex core emerging from the nozzle and the corresponding tangential velocity distribution are also controlling factors. Excitability of swirling jets is also investigated by exciting a flow with a swirl number of 0.35 by plane acoustic waves at a constant sound pressure level and at various frequencies. It is observed that the cold swirling jet is excitable by plane waves, and that the instability waves grow about 50 percent less in peak r.m.s. amplitude and saturate further upstream compared to corresponding waves in a jet without swirl having the same axial mass flux. The preferred Strouhal number based on the mass-averaged axial velocity and nozzle exit diameter for both swirling and nonswirling flows is 0.4. Taghavi, Rahmat and Farokhi, Saeed Unspecified Center NASA-CR-180895, NAS 1.26:180895 NCC3-56; RTOP 505-62-21...

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
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Category : Government publications
Languages : en
Pages : 1644

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1200

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Government reports annual index

Government reports annual index PDF Author:
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Category :
Languages : en
Pages : 1420

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Coastal Engineering Journal PDF Author:
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Category : Coast changes
Languages : en
Pages : 438

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Covers coastal, harbor and offshore engineering.

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NASA Conference Publication PDF Author:
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 522

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Category : Science
Languages : en
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The Finding Guide to AIAA Meeting Papers

The Finding Guide to AIAA Meeting Papers PDF Author: American Institute of Aeronautics and Astronautics. Technical Information Service
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 764

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