3 edition of High-accuracy compact MacCormack-type schemes for computational aeroacoustics found in the catalog.
High-accuracy compact MacCormack-type schemes for computational aeroacoustics
Published
1998
by National Aeronautics and Space Administration, Lewis Research Center, National Technical Information Service [distributor in Cleveland, Ohio, Springfield, VA
.
Written in English
Edition Notes
| Other titles | High accuracy compact MacCormack type schemes for computational aeroacoustics. |
| Statement | R. Hixon, E. Turkel. |
| Series | [NASA contractor report] -- NASA/CR-1998-208672., NASA contractor report -- NASA CR-208672. |
| Contributions | Turkel, E., Lewis Research Center. |
| The Physical Object | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL15547001M |
Computational Partial Differential Equations Using MATLAB® In many application areas, such as aeroacoustics [12, 13, 26, 30] and electromagnetics [24], the propagation of acoustic and electromagnetic waves needs to be accurately simulated over very long periods of time and far distances. Experience has shown that compact schemes are. Full text of "An Automated Code Generator for Three-Dimensional Acoustic Wave Propagation with Geometrically Complex Solid Wall Boundaries" See other formats.
Y. NASA Conference Publication ong>Secondong> ong>Computationalong> ong>Aeroacousticsong> (ong>CAAong>) ong>Workshopong> on . Analysis of a new high resolution upwind compact scheme - Free download as PDF File .pdf), Text File .txt) or read online for free. Upwind compact scheme.
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Recently,anewclass of high-accuracy explicit MacCormack-type schemes have been intro- duced for computational aeroacoustics. 6 Applying this methodology to compact schemes has resulted in a new class of compact MacCormack-type schemes which use three-point stencils.
High-accuracy compact MacCormack-type schemes for computational aeroacoustics (SuDoc NAS ) [R. Hixon] on johnsonout.com *FREE* shipping on qualifying johnsonout.com: R. Hixon. High-accuracy compact MacCormack-type schemes for computational aeroacoustics [microform] / R. Hixon, E.
Turkel National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service [distributor Cleveland, Ohio: Springfield, VA Australian/Harvard Citation.
Hixon, R. & Turkel, E. & Lewis Research. Note: Citations are based on reference standards. However, formatting rules can vary widely between applications and fields of interest or study.
The specific requirements or preferences of your reviewing publisher, classroom teacher, institution or organization should be applied. Compact Implicit MacCormack-Type Schemes with High Accuracy Article in Journal of Computational Physics (1) · February with Reads How we measure 'reads'.
A comprehensive guide to the developments in the field of computational aeroacoustics—a research field that deals with sound generated by unsteady flows, found in the noise generated by aircraft—this book provides academic and corporate researchers with a concise overview of the field while acting as a launch pad for additional study.
Download A comprehensive guide to the developments in the field of computational aeroacoustics—a research field that deals with sound generated by unsteady flows, found in the noise generated by aircraft—this book provides academic and corporate researchers with a concise overview of the field while acting as a launch pad for additional study.
High-Accuracy Compact MacCormack-Type Schemes for Computational Aeroacoustics eBook: National Aeronautics and Space Administration NASA: johnsonout.com: Kindle StoreAuthor: National Aeronautics and Space Administration NASA.
Buy High-accuracy compact MacCormack-type schemes for computational aeroacoustics (NASA/CR-) by R. R Hixon (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible johnsonout.com: R. R Hixon.
High-Accuracy Large-Step Explicit Runge-Kutta (HALE-RK) Schemes for Computational Aeroacoustics Article in Journal of Computational Physics (10) · June with Reads. Nov 30, · Parameter optimization is an excellent path for easily raising the resolution efficiency of compact finite differencing schemes.
Their low-resolution errors are attractive for resolving the fine-scale turbulent physics even in complex flow domains with difficult boundary johnsonout.com by: 2. The Stability of Numerical Boundary Treatments for Compact High-Order Finite-Difference Schemes,” Second Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, Hampton, VA, NASA CP 6.
Hixon, R., and. Turkel, E.,“ High-Accuracy Compact MacCormack-Type Schemes for Computational Aeroacoustics,” Report NASA∕CR Cited by: 1. Computational Science and Its Applications – ICCSA International Conference on Computational Science and Its Applications.
ICCSA Computational Science and Its Applications – Cited by: 5. We're upgrading the ACM DL, and would like your input. Please sign up to review new features, functionality and page johnsonout.com by: 5.
The fan interaction noise is modeled as an annular cascade in terms of the Euler equations linearized about a nonuniform rotational flow. The model accounts for the inflow-fan-duct coupling and the high frequency of the interaction johnsonout.com by: 4. Procedia Engineering 00 () 1–10 Procedia Engineering IUTAM Symposium on Computational Aero-Acoustics for Aircraft Noise Prediction Modeling Tonal and Broadband Interaction Noise H.
Atassi, M. Logue University of Notre Dame Notre Dame, INUSA Abstract The fan interaction noise is modeled as an annular cascade in terms of the Euler equations linearized about a nonuniform Cited by: 8.
Abstract. The paper provides an overview on the use of high-resolution methods based on the CABARET scheme. The results are provided for several test problems including gas dynamics, computational aeroacoustics, and geophysical fluid dynamics for a classical double-gyre quasi-geostrophic model of ocean johnsonout.com by: 2.
page 1 a finite volume, cartesian grid method for computational aeroacoustics by mihaela popescu a dissertation presented to the graduate school of the university of flor ida in partial fulfillment of the requirements for the degree of doctor of philosophy university of florida Full text of "Second Computational Aeroacoustics (CAA) Workshop on Benchmark Problems" See other formats.
Runge-Kutta (HALE-RK) schemes for computational aeroacoustics, Journal of Computational G. and Zhang, X., Optimized prefactored compact schemes, Journal of Computational Physics, Vol. pp. Compact implicit MacCormack-type schemes with high accuracy, Journal of Computational Physics, Vol.
pp. [12 Cited by: 4. Abstract The fan interaction noise is modeled as an annular cascade in terms of the Euler equations linearized about a nonuniform rotational flow.
The model accounts for the inflow-fan-duct coupling and the high frequency of the interaction process. An efficient split velocity formulation is developed, making it suitable for broadband calculations.Stanford Libraries' official online search tool for books, media, journals, databases, government documents and more.Achetez et téléchargez ebook High-Accuracy Compact MacCormack-Type Schemes for Computational Aeroacoustics (English Edition): Boutique Kindle - Science: johnsonout.comat: Format Kindle.
