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Improved Finite Element Modeling Of The Turbofan Engine Inlet Radiation Problem by Indranil Danda Roy
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1NASA Technical Reports Server (NTRS) 19970017415: Improved Finite Element Modeling Of The Turbofan Engine Inlet Radiation Problem
By NASA Technical Reports Server (NTRS)
Improvements have been made in the finite element model of the acoustic radiated field from a turbofan engine inlet in the presence of a mean flow. The problem of acoustic radiation from a turbofan engine inlet is difficult to model numerically because of the large domain and high frequencies involved. A numerical model with conventional finite elements in the near field and wave envelope elements in the far field has been constructed. By employing an irrotational mean flow assumption, both the mean flow and the acoustic perturbation problem have been posed in an axisymmetric formulation in terms of the velocity potential; thereby minimizing computer storage and time requirements. The finite element mesh has been altered in search of an improved solution. The mean flow problem has been reformulated with new boundary conditions to make it theoretically rigorous. The sound source at the fan face has been modeled as a combination of positive and negative propagating duct eigenfunctions. Therefore, a finite element duct eigenvalue problem has been solved on the fan face and the resulting modal matrix has been used to implement a source boundary condition on the fan face in the acoustic radiation problem. In the post processing of the solution, the acoustic pressure has been evaluated at Gauss points inside the elements and the nodal pressure values have been interpolated from them. This has significantly improved the results. The effect of the geometric position of the transition circle between conventional finite elements and wave envelope elements has been studied and it has been found that the transition can be made nearer to the inlet than previously assumed.
“NASA Technical Reports Server (NTRS) 19970017415: Improved Finite Element Modeling Of The Turbofan Engine Inlet Radiation Problem” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19970017415: Improved Finite Element Modeling Of The Turbofan Engine Inlet Radiation Problem
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19970017415: Improved Finite Element Modeling Of The Turbofan Engine Inlet Radiation Problem” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - FINITE ELEMENT METHOD - SOUND WAVES - FAR FIELDS - TURBOFAN ENGINES - ENGINE INLETS - MATHEMATICAL MODELS - DIGITAL SIMULATION - COMPUTERIZED SIMULATION - NUMERICAL FLOW VISUALIZATION - ACOUSTICS - COMPUTATIONAL FLUID DYNAMICS - BOUNDARY CONDITIONS - NEAR FIELDS - POTENTIAL FLOW - EIGENVALUES - COMPUTATIONAL GRIDS - GAUSS EQUATION - Roy, Indranil Danda - Eversman, Walter - Meyer, H. D.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19970017415
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 92.97 Mbs, the file-s for this book were downloaded 64 times, the file-s went public at Tue Oct 04 2016.
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1Woodcraft Boys at Sunset Island
By May Folwell Hoisington and Lillian Elizabeth Roy

An adventure story for boys, it was included in the Every Boys' Library, a collection of works deemed the most popular among boys. Set on an island off the coast of Maine, Woodcraft Boys at Sunset Island is an account of several school-age children and their parents as they explore nature and learn survival skills. They go on adventures, encounter thieves, find a pig on a raft, and through it all, learn the value of self-reliance. (JayKitty76)
“Woodcraft Boys at Sunset Island” Metadata:
- Title: ➤ Woodcraft Boys at Sunset Island
- Authors: May Folwell HoisingtonLillian Elizabeth Roy
- Language: English
- Publish Date: 1919
Edition Specifications:
- Format: Audio
- Number of Sections: 14
- Total Time: 05:44:12
Edition Identifiers:
- libriVox ID: 12801
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- File Name: woodcraftboys_sunsetisland_1810_librivox
- File Format: zip
- Total Time: 05:44:12
- Download Link: Download link
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