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BBT Side Mold Assy M02D Rendered 02Hemphill, Bill 01 January 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1007/thumbnail.jpg
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BBT Side Mold Assy Pen Small 01Hemphill, Bill 01 January 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1008/thumbnail.jpg
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Gluing KerfingHemphill, Bill 28 October 2021 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1009/thumbnail.jpg
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Screenshot 3D Pen BBT Side Mold Assy M02D with SpreaderHemphill, Bill 01 January 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1010/thumbnail.jpg
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Screenshot BBT Side Mold Assy M02D RC02Hemphill, Bill 07 June 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1011/thumbnail.jpg
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Screenshot CNC Toolpaths BBT Side Mold Assy M02D RC02Hemphill, Bill 07 June 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1012/thumbnail.jpg
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Screenshot Dimensions BBT Side Mold Assy M02D RC02Hemphill, Bill 07 June 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1013/thumbnail.jpg
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Screenshot Drill Template BBT Side Mold Assy M02D RC02Hemphill, Bill 07 June 2022 (has links)
https://dc.etsu.edu/oer-guitars-images-complete/1014/thumbnail.jpg
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Coupled thermal-fluid analysis with flowpath-cavity interaction in a gas turbine engineFitzpatrick, John Nathan 12 1900 (has links)
Indiana University-Purdue University Indianapolis (IUPUI) / This study seeks to improve the understanding of inlet conditions of a large rotor-stator cavity in a turbofan engine, often referred to as the drive cone cavity (DCC). The inlet flow is better understood through a higher fidelity computational fluid dynamics (CFD) modeling of the inlet to the cavity, and a coupled finite element (FE) thermal to CFD fluid analysis of the cavity in order to accurately predict engine component temperatures. Accurately predicting temperature distribution in the cavity is important because temperatures directly affect the material properties including Young's modulus, yield strength, fatigue strength, creep properties. All of these properties directly affect the life of critical engine components. In addition, temperatures cause thermal expansion which changes clearances and in turn affects engine efficiency. The DCC is fed from the last stage of the high pressure compressor. One of its primary functions is to purge the air over the rotor wall to prevent it from overheating. Aero-thermal conditions within the DCC cavity are particularly challenging to predict due to the complex air flow and high heat transfer in the rotating component. Thus, in order to accurately predict metal temperatures a two-way coupled CFD-FE analysis is needed. Historically, when the cavity airflow is modeled for engine design purposes, the inlet condition has been over-simplified for the CFD analysis which impacts the results, particularly in the region around the compressor disc rim. The inlet is typically simplified by circumferentially averaging the velocity field at the inlet to the cavity which removes the effect of pressure wakes from the upstream rotor blades. The way in which these non-axisymmetric flow characteristics affect metal temperatures is not well understood. In addition, a constant air temperature scaled from a previous analysis is used as the simplified cavity inlet air temperature. Therefore, the objectives of this study are: (a) model the DCC cavity with a more physically representative inlet condition while coupling the solid thermal analysis and compressible air flow analysis that includes the fluid velocity, pressure, and temperature fields; (b) run a coupled analysis whose boundary conditions come from computational models, rather than thermocouple data; (c) validate the model using available experimental data; and (d) based on the validation, determine if the model can be used to predict air inlet and metal temperatures for new engine geometries.
Verification with experimental results showed that the coupled analysis with the 3D no-bolt CFD model with predictive boundary conditions, over-predicted the HP6 offtake temperature by 16k. The maximum error was an over-prediction of 50k while the average error was 17k. The predictive model with 3D bolts also predicted cavity temperatures with an average error of 17k. For the two CFD models with predicted boundary conditions, the case without bolts performed better than the case with bolts. This is due to the flow errors caused by placing stationary bolts in a rotating reference frame. Therefore it is recommended that this type of analysis only be attempted for drive cone cavities with no bolts or shielded bolts.
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OpenFlow based load balancing and proposed theory for integration in VoIP networkPandita, Shreya 21 May 2014 (has links)
Indiana University-Purdue University Indianapolis (IUPUI) / In today's internet world with such a high traffic, it becomes inevitable to have multiple servers representing a single logical server to share enormous load. A very common network configuration consists of multiple servers behind a load balancer. The load balancer determines which server would service a clients request or incoming load from the client. Such a hardware is expensive, runs a fixed policy or algorithm and is a single point of failure. In this paper, we will implement and analyze an alternative load balancing architecture using OpenFlow. This architecture acquires flexibility in policy, costs less and has the potential to be more robust. This paper also discusses potential usage of OpenFlow based load balancing for media gateway selection in SIP-PSTN networks to improve VoIP performance.
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