ICASE/LaRC Workshop on Benchmark Problems in Computational Aeroacoustics (CAA) PDF Download
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Author: Jay C. Hardin
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 412
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Book Description
Author: Jay C. Hardin
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 412
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Book Description
Author: J. C. Hardin
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 397
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Book Description
Author: J. C. Hardin
Publisher:
ISBN:
Category : Numerical analysis
Languages : en
Pages : 397
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Book Description
Author: C. K. W. Tam
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 396
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 408
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Book Description
Author: Christopher K.W. Tam
Publisher:
ISBN:
Category :
Languages : en
Pages : 380
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 652
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721684908
Category :
Languages : en
Pages : 34
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Book Description
NASA has conducted a series of Computational Aeroacoustics (CAA) Workshops on Benchmark Problems to develop a set of realistic CAA problems that can be used for code validation. In the Third (1999) and Fourth (2003) Workshops, the single airfoil gust response problem, with real geometry effects, was included as one of the benchmark problems. Respondents were asked to calculate the airfoil RMS pressure and far-field acoustic intensity for different airfoil geometries and a wide range of gust frequencies. This paper presents the validated that have been obtained to the benchmark problem, and in addition, compares them with classical flat plate results. It is seen that airfoil geometry has a strong effect on the airfoil unsteady pressure, and a significant effect on the far-field acoustic intensity. Those parts of the benchmark problem that have not yet been adequately solved are identified and presented as a challenge to the CAA research community. Scott, James R. Glenn Research Center NASA/TM-2004-213386, IMECE2004-59865, E-14894
Author: C. K. W. Tam
Publisher:
ISBN:
Category : Sound
Languages : en
Pages : 380
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Book Description
Author: Tapan Sengupta
Publisher: Cambridge University Press
ISBN: 1107023637
Category : Computers
Languages : en
Pages : 589
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Book Description
""Presents methods necessary for high accuracy computing of fluid flow and wave phenomena in single source format using unified spectral theory of computing"--Provided by publisher"--
