Integrated Simulation/Design/Analysis Infrastructure for SiC-based High-Temperature Power Conversion

Posted by on Oct 24, 2009 in Charles Eric Lucas, Contracts, Electronics, SBIR Phase I, SBIR Phase II, Thermal Systems | 0 comments

Type of Awards: SBIR Phase I with IEDC and Phase II Contract Numbers: FA8650-05-M-2599 and FA8650-06-C-2663 Agency: U.S. Air Force Research Laboratory Status: Completed Periods: 4/1/05 to 1/1/06 and 5/5/06 to 9/5/08 Principal Investigator: C. E. Lucas Abstract: In order to realize the full potential of Silicon Carbide and to facilitate its deployment in high-temperature power electronics applications, it is important to establish an integrated modeling, simulation, and analysis (MS&A) infrastructure to address the special considerations and numerous technical challenges that must be overcome and to support design at the device, subsystem, and system levels.  The viability of such an infrastructure has been established in the on-going Phase I research.  The overall objective of the proposed Phase II research is to further its development.  In particular, the proposed Phase II effort entails: (1) the continued development of a distributed multi-level (device/subsystem/system) integrated (electrical/thermal) MS&A infrastructure to support SiC device development and their application to Air Force systems, (2) the investigation of how SiC device performance is affected by thermal and material properties and how defects influence thermal-electrical coupling, (3) the partitioning of the geometric physics-based device models for implementation in a distributed computer network, and (4) the investigation of the applicability of this powerful MS&A infrastructure to other areas of interest such as computational fluid dynamics, plasma physics, and...

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Advanced Heat Exchanger (HEX) Scaling Methodologies for High-Performance Aircraft

Posted by on Oct 24, 2009 in Alex Heltzel, Contracts, SBIR Phase I, SBIR Phase II, Thermal Systems | 0 comments

Type of Awards: SBIR Phase I and Phase II Subcontractors: Mezzo Technologies  and Honeywell Aerospace Contract Numbers: FA8650-08-M-2843 and FA8650-09-C-2400 Agency: U.S. Air Force Research Laboratory Status: On Going Periods: 9/18/07 to 9/18/08 and 5/28/09 to 9/13/11 Principal Investigator: A. Heltzel Abstract: The current thermal management effort for high performance aircraft focuses much attention on more efficient energy rejection through the development of advanced heat exchanger technologies. PC Krause and Associates (PCKA) is currently filling a much-needed gap of scaling and performance knowledge in the Air Force Phase I SBIR effort. 3-D computational fluid dynamics models have been constructed, which have been shown to accurately predict microstructured heat sink performance where conventional analysis methods fail. The ability to collapse high-fidelity data into a performance database is allowing PCKA to develop a rapid analysis software package for advanced heat exchangers. In Phase II, PCKA will team with both Honeywell Aerospace and Mezzo Technologies Inc., two manufacturers of candidate heat exchangers. This collaboration will enable the application of the analysis tool to near-term heat exchanger design projects, in addition to providing validation, manufacturing, and non-core effect information to the analysis method. PCKA will expand the modeling and simulation effort to encompass additional heat exchanger designs, materials, working fluids, operating conditions, and the true dynamic response of candidate heat exchangers. The software tool to be developed in Phase II directly addresses the stated goal of this project: accelerating the design concept to development to fabrication...

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Efficient Multi-Scale Radiation Transport Modeling

Posted by on Oct 24, 2009 in Alex Heltzel, Contracts, SBIR Phase I, Thermal Systems | 0 comments

Type of Awards: SBIR Phase I Contract Numbers: NNX09CF07P Agency: NASA Glenn Research Center Status: On Going Periods: 1/22/09 to 7/22/09 Principal Investigator: A. Heltzel Abstract: Focusing on a reduced-dimension problem of a hypersonic orbital/lunar reentry capsule, an algorithm will be built which combines the stochastic Monte Carlo method for treatment of radiation transport in optically thin to moderate domains, with a single-term modified differential approximation (MP1) for use in optically thick domains.  This numerical method will be verified against a known benchmark case before application to the reentry problem.  The bandwise and cumulative distribution function (CDF) methods will be combined within the Monte Carlo framework, creating an efficient, dual-hybrid radiation transport algorithm.  A detailed plan for the generation of the full algorithm will be developed, with a focus on parallelization and compatibility with existing commercial transport software.  This plan will include thorough testing and validation...

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Simulation of Electromagnetic Field Distribution at a Nanowire Probe for Near Field Scanning Optical Microscopy

Posted by on Oct 22, 2009 in Alex Heltzel, Publications, Thermal Systems | 0 comments

N. P. Malcolm, Department of Mechanical Engineering, University of Texas at Austin; A. Heltzel, PC Krause and Associates, Inc; L. Shi, J. R. Howell, Department of Mechanical Engineering, University of Texas at Austin ASME Micro/Nanoscale Heat Transfer International Conference, Tainan, Taiwan, 2008.

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Dynamic Thermal Management System Modeling of a More Electric Aircraft

Posted by on Oct 22, 2009 in Aircraft, Alex Heltzel, Eric A. Walters, Publications, Thermal Systems | 0 comments

K. McCarthy, E. A. Walters, A. Heltzel, PC Krause and Associates, Inc;  R. Elangovan, G. Roe, W. Vannice, Boeing;  C. Schemm, Lockheed Martin;   J. Dalton, Avetec;      S. Iden, P. Lamm, C. Miller, U.S. Air Force Research Laboratory;  A. Susainathan, U.S. Air Force Aeronautical Systems Center Advancements in electrical, mechanical, and structural design onboard modern more electric aircraft have added significant stress to the thermal management systems (TMS). A thermal management system level analysis tool has been created in MATLAB/Simulink to facilitate rapid system analysis and optimization to meet the growing demands of modern aircraft. It is anticipated that the tracking of thermal energy through numerical integration will lead to more accurate predictions of worst case TMS sizing conditions. In addition, the nonproprietary nature of the tool affords users the ability to modify component models and integrate advanced conceptual designs that can be evaluated over multiple missions to determine the impact at a system level. 2008 SAE Power Systems Conference, November 11-13 2008, Bellevue,  WA. Paper...

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Simulation of a Plasmonic Tip-Terminated Scanning Nanowire Waveguide for Molecular Imaging

Posted by on Oct 22, 2009 in Alex Heltzel, Publications, Thermal Systems | 0 comments

Nathan P. Malcolm, Department of Mechanical Engineering, University of Texas at Austin; A. Heltzel, PC Krause and Associates, Inc; Konstantin V. Sokolov, Department of Biomedical Engineering, University of Texas M.D. Anderson Cancer Center; Li Shi and John R. Howell, Department of Mechanical Engineering, University of Texas at Austin Finite difference time domain simulation reveals plasmonic coupling and local field enhancement at the gap between the gold nanoparticle _NP_ tip of a ZnO nanowire _NW_ waveguide and a gold-coated substrate or a gold NP probe. The region of field enhancement is about three times smaller than the 100 nm diameter of the gold NP tip, making the NW waveguide grown on a transparent microcantilever well-suited for near field imaging of single molecules immobilized on a gold substrate or gold NP-labeled cell membranes with superior spatial resolution and signal to noise ratio. 2008 American Institute of Physics. _DOI:...

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