Simulation, Characterization and Control of Forced Unsteady Viscous Flows Using Navier-Stokes Equations

Simulation, Characterization and Control of Forced Unsteady Viscous Flows Using Navier-Stokes Equations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 139

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Book Description
A two-and-a-quarter-year multi-tasked research project was pursued by the present investigators to study dynamic stall phenomenon under AFOSR sponsorship between February 1990 - May 1992. The major objective of this study was to predict and control the dynamic stall phenomenon in 2-D and 3-D flows. In the process of achieving these objectives, significant effort was directed towards developing mathematical models and the corresponding computational methods which were made available to interested researchers and organizations involved in computational fluid dynamics (CFD) research. The analyses developed included a two-dimensional Navier-Stokes (NS) analysis for a general body undergoing arbitrary three-degree-of-freedom maneuvers; detailed results are provided for this class of flows. For enhancement of accuracy and efficiency, an adaptive-grid time-accurate flow solution technique has been developed to enable improved resolution of the various length scales in a vortex-dominated unsteady flow. A multi-block grid generation analysis is developed for a 3-D rectangular planform wing. For the corresponding flow analysis using velocity-vorticity variables and direct-solution philosophy, the difficulties experienced were clearly discussed in the annual report submitted a year ago in November 1991. This 3-D flow analysis was therefore temporarily set aside. It will be pursued further in a subsequent grant, and the progress made on it will be reported in a forthcoming annual report for that grant. In the current grant, the study of 3-D flows was continued, using an iterative solution methodology. Hence, a 3-D unsteady Navier-Stokes analysis, again using velocity-vorticity variables, and an iterative solution technique with multi-grid acceleration have been developed.

Simulation, Characterization and Control of Forced Unsteady Viscous Flows Using Navier-Stokes Equations

Simulation, Characterization and Control of Forced Unsteady Viscous Flows Using Navier-Stokes Equations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 139

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Book Description
A two-and-a-quarter-year multi-tasked research project was pursued by the present investigators to study dynamic stall phenomenon under AFOSR sponsorship between February 1990 - May 1992. The major objective of this study was to predict and control the dynamic stall phenomenon in 2-D and 3-D flows. In the process of achieving these objectives, significant effort was directed towards developing mathematical models and the corresponding computational methods which were made available to interested researchers and organizations involved in computational fluid dynamics (CFD) research. The analyses developed included a two-dimensional Navier-Stokes (NS) analysis for a general body undergoing arbitrary three-degree-of-freedom maneuvers; detailed results are provided for this class of flows. For enhancement of accuracy and efficiency, an adaptive-grid time-accurate flow solution technique has been developed to enable improved resolution of the various length scales in a vortex-dominated unsteady flow. A multi-block grid generation analysis is developed for a 3-D rectangular planform wing. For the corresponding flow analysis using velocity-vorticity variables and direct-solution philosophy, the difficulties experienced were clearly discussed in the annual report submitted a year ago in November 1991. This 3-D flow analysis was therefore temporarily set aside. It will be pursued further in a subsequent grant, and the progress made on it will be reported in a forthcoming annual report for that grant. In the current grant, the study of 3-D flows was continued, using an iterative solution methodology. Hence, a 3-D unsteady Navier-Stokes analysis, again using velocity-vorticity variables, and an iterative solution technique with multi-grid acceleration have been developed.

Simulation, Characteriation and Control of Forced Unsteady Viscous Flows Using Navier-Stokes Equations

Simulation, Characteriation and Control of Forced Unsteady Viscous Flows Using Navier-Stokes Equations PDF Author: Kirti N. Ghia
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 140

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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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Unsteady Viscous Flows

Unsteady Viscous Flows PDF Author: Demetri P. Telionis
Publisher: Springer
ISBN:
Category : Science
Languages : en
Pages : 440

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 348

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An Unstructured Grid Generation and Adaptive Solution Technique for High-Reynolds-number Compressible Flows

An Unstructured Grid Generation and Adaptive Solution Technique for High-Reynolds-number Compressible Flows PDF Author: Gregory Allan Ashford
Publisher:
ISBN:
Category :
Languages : en
Pages : 500

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 492

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538

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Numerical Experiments in Unsteady Flows Through the Use of Full Navier- Stokes Equations

Numerical Experiments in Unsteady Flows Through the Use of Full Navier- Stokes Equations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 149

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Book Description
The numerical simulations of impulsively started flow, non- impulsively started flow, sinusoidally oscillating flow, and, finally, co- existing flow (with mean and oscillatory components) past a circular cylinder have been investigated in great detail through the use of several compact schemes with the Navier-Stokes vorticity/stream function formulation for various Reynolds numbers, frequency parameters, and ambient flow/oscillating flow combinations using VAX-3520 and NASA's Supercomputers. Extensive sensitivity analysis has been performed to delineate the effects of time step, outer boundary, nodal points on the cylinder, and the use of higher order polynomials in the calculation of the gradient of wall vorticity. The results have been compared with those obtained experimentally. In many cases the predicted wake region, vorticity and pressure distributions, and the time-variation of the force coefficients have shown excellent agreement with those obtained experimentally.

NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 590

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