Author:
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 30
Book Description
Flowfield of a Lifting Hovering Rotor: A Navier-Stokes Simulation
Author:
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 30
Book Description
Navier-Stokes Flowfield Computation of Wing/rotor Interaction for a Tilt Rotor Aircraft in Hover
Author: Ian G. Fejtek
Publisher:
ISBN:
Category :
Languages : en
Pages : 162
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 162
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 866
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 866
Book Description
Research in Progress
Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 274
Book Description
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 274
Book Description
An Overset Grid Navier-Stokes/Kirchhoff-surface Method for Rotorcraft Aeroacoustic Predictions
Author: Earl P. N. Duque
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 20
Book Description
Abstract: "This paper describes a new method for computing the flowfield and acoustic signature of arbitrary rotors in forward flight. The overall scheme uses a finite-difference Navier-Stokes solver to compute the aerodynamic flowfield near the rotor blades. The equations are solved on a system of overset grids that allow for prescribed cyclic and flapping blade motions and capture the interactions between the rotor blades and wake. The far-field noise is computed with a Kirchhoff integration over a surface that completely encloses the rotor blades. Flowfield data are interpolated onto this Kirchhoff surface using the same overset-grid techniques that are used for the flowfield solution. As a demonstration of the overall prediction scheme, computed results for far-field noise are compared with experimental data for both high-speed impulsive (HSI) and blade-vortex interaction (BVI) cases. The HSI case showed good agreement with experimental data while a preliminary attempt at the BVI case did not. The computations clearly show that temporal accuracy, spatial accuracy and grid resolution in the Navier-Stokes solver play key roles in the overall accuracy of the predicted noise. These findings will be addressed more closely in future BVI computations. Overall, the overset-grid CFD scheme provides a powerful new framework for the prediction of helicopter noise."
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 20
Book Description
Abstract: "This paper describes a new method for computing the flowfield and acoustic signature of arbitrary rotors in forward flight. The overall scheme uses a finite-difference Navier-Stokes solver to compute the aerodynamic flowfield near the rotor blades. The equations are solved on a system of overset grids that allow for prescribed cyclic and flapping blade motions and capture the interactions between the rotor blades and wake. The far-field noise is computed with a Kirchhoff integration over a surface that completely encloses the rotor blades. Flowfield data are interpolated onto this Kirchhoff surface using the same overset-grid techniques that are used for the flowfield solution. As a demonstration of the overall prediction scheme, computed results for far-field noise are compared with experimental data for both high-speed impulsive (HSI) and blade-vortex interaction (BVI) cases. The HSI case showed good agreement with experimental data while a preliminary attempt at the BVI case did not. The computations clearly show that temporal accuracy, spatial accuracy and grid resolution in the Navier-Stokes solver play key roles in the overall accuracy of the predicted noise. These findings will be addressed more closely in future BVI computations. Overall, the overset-grid CFD scheme provides a powerful new framework for the prediction of helicopter noise."
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 664
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 664
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Wind Turbine Aerodynamics
Author: J. F. Brouckaert
Publisher:
ISBN:
Category : Wind turbines
Languages : en
Pages : 606
Book Description
Publisher:
ISBN:
Category : Wind turbines
Languages : en
Pages : 606
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1638
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1638
Book Description