Author: Ching Yuen Loh
Publisher:
ISBN:
Category :
Languages : en
Pages : 6
Book Description
Gap noise computation by the CE/SE method
Author: Ching Yuen Loh
Publisher:
ISBN:
Category :
Languages : en
Pages : 6
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 6
Book Description
GAP Noise Computation By The CE/SE Method
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Gap Noise Computation by the Ce
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Computation of Feedback Aeroacoustic System by the CE/SE Method
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
Computational Aeroacoustics by the Space-Time CE/SE Method
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 932
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 932
Book Description
Computational Fluid Dynamics 2000
Author: Nobuyuki Satofuka
Publisher: Springer Science & Business Media
ISBN: 3642565352
Category : Science
Languages : en
Pages : 807
Book Description
These proceedings contain a selection of refereed contributions as a source of reference for all those interested in the state of the art in computational fluid dynamics. The conference brings together physicists, mathematicians and engineers to review and share recent advances in the field.
Publisher: Springer Science & Business Media
ISBN: 3642565352
Category : Science
Languages : en
Pages : 807
Book Description
These proceedings contain a selection of refereed contributions as a source of reference for all those interested in the state of the art in computational fluid dynamics. The conference brings together physicists, mathematicians and engineers to review and share recent advances in the field.
Near Field Trailing Edge Tone Noise Computation
Author: Ching Y. Loh
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
AIAA Aerospace Sciences Meeting and Exhibit, 42nd
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562
Book Description
Near Field Trailing Edge Tone Noise Computation
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721534289
Category :
Languages : en
Pages : 28
Book Description
Blunt trailing edges in a flow often generate tone noise due to wall-jet shear layer and vortex shedding. In this paper, the space-time conservation element (CE/SE) method is employed to numerically study the near-field noise of blunt trailing edges. Two typical cases, namely, flow past a circular cylinder (aeolian noise problem) and flow past a flat plate of finite thickness are considered. The computed frequencies compare well with experimental data. For the aeolian noise problem, comparisons with the results of other numerical approaches are also presented. Loh, Ching Y. Glenn Research Center NASA/CR-2002-212013, NAS 1.26:212013, E-13703, AIAA Paper 2003-0365
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721534289
Category :
Languages : en
Pages : 28
Book Description
Blunt trailing edges in a flow often generate tone noise due to wall-jet shear layer and vortex shedding. In this paper, the space-time conservation element (CE/SE) method is employed to numerically study the near-field noise of blunt trailing edges. Two typical cases, namely, flow past a circular cylinder (aeolian noise problem) and flow past a flat plate of finite thickness are considered. The computed frequencies compare well with experimental data. For the aeolian noise problem, comparisons with the results of other numerical approaches are also presented. Loh, Ching Y. Glenn Research Center NASA/CR-2002-212013, NAS 1.26:212013, E-13703, AIAA Paper 2003-0365