A Numerical Investigation of Laminar Confined Coaxial Jet Flow

A Numerical Investigation of Laminar Confined Coaxial Jet Flow PDF Author: Harold E. Adkins
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 360

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A Numerical Investigation of Laminar Confined Coaxial Jet Flow

A Numerical Investigation of Laminar Confined Coaxial Jet Flow PDF Author: Harold E. Adkins
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 360

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Turbulent Mixing in the Initial Region of Heterogeneous Axisymmetric Coaxial Confined Jets

Turbulent Mixing in the Initial Region of Heterogeneous Axisymmetric Coaxial Confined Jets PDF Author: Kirti N. Ghia
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 100

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Scientific and Technical Aerospace Reports

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

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Numerical Investigation of the Laminar, Supersonic Flow Over a Rearward-facing Step Using an Adaptive Grid Scheme

Numerical Investigation of the Laminar, Supersonic Flow Over a Rearward-facing Step Using an Adaptive Grid Scheme PDF Author: Stephen Corda
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 218

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Numerical Investigation of a Jet Flow with a Hatch and an Opening

Numerical Investigation of a Jet Flow with a Hatch and an Opening PDF Author: Mrinal V.. Nagrecha
Publisher:
ISBN:
Category : Electronic dissertations
Languages : en
Pages : 68

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The goal of this project was to establish a datum for acoustics generated in an exhaust flow from a jet pipe, due to the presence of an opening with a hatch at an angle, by using the Computational Fluid Dynamics (CFD) tool FLUENT. After validating the geometry using a supersonic case employing a fully expanded jet, a secondary supersonic test case was produced to compare results with the former using a Detached Eddy Simulation with Spalart-Allmaras (DES-SA) scheme. Two subsonic cases using the same boundary conditions (BCs) were then computed using a Large Eddy Simulation (LES) turbulence model in order to solve for flow-field data and Sound Pressure Level (SPL) of the given geometry. Focus was given to the region around the opening, and the computed pressure data was stored in three regions: above the opening, under the opening, and past the opening. Pressure contours in the region around the hatch were captured well and shown to be consistent between the two geometries employed for the domain of solution. Results concluded that using the smaller domain of solution maintained resolution quality while decreasing overall computation time tremendously.

Applied mechanics reviews

Applied mechanics reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 400

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Experimental Study of One- and Two-component Low-turbulence Confined Coaxial Flows

Experimental Study of One- and Two-component Low-turbulence Confined Coaxial Flows PDF Author: John C. Bennett
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 100

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International Aerospace Abstracts

International Aerospace Abstracts PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 974

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Numerical Investigation of Laminar and Turbulent Natural Convection in Enclosures

Numerical Investigation of Laminar and Turbulent Natural Convection in Enclosures PDF Author: Gregory P. Nurnberg
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 244

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Hydraulic Research in the United States and Canada

Hydraulic Research in the United States and Canada PDF Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 1046

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