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Hybrid Vorticity Transport Method for Rotorcraft Comprehensive Analysis
- Small Business Information
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Woman-Owned: NoMinority-Owned: NoHUBZone-Owned: No
- Phase 1
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Fiscal Year: 2009Title: Hybrid Vorticity Transport Method for Rotorcraft Comprehensive AnalysisAgency / Branch: DOD / ARMYContract: W911W6-10-C-0018Award Amount: $69,983.00
Abstract:
The overall objective of this proposal is to develop a standalone module for efficient LES of incompressible and transonic flow of rotorcraft wake on a distributed network of multicore CPUs and GPUs. The module will be based on a Lagrangian Vortex Particle Method (LVPM) and will include the capability to interface with other CFD codes, using Python or a similarly versatile language. The interface will be developed with "code agnosticism" in mind, allowing it to exchange requisite input/output variables and parameters between the LVPM and arbitrary external CFD solvers. A compressibility model will be introduced to LVPM to allow for a more natural interface with compressible CFD codes. Novel software and hardware technologies will be implemented to substantially accelerate the simulation turn around times. Phase I will involve implementation of LES on a cluster of GPUs, interfacing LVPM with a well-established CFD code, and demonstrating proof of concept using a number of test problems.Small Business Information at Submission:APPLIED SCIENTIFIC RESEARCH
1800 East Garry Ave, Suite 214 Santa Ana, CA 92705EIN/Tax ID: 330832615DUNS: N/ANumber of Employees:Woman-Owned: NoMinority-Owned: NoHUBZone-Owned: No
Award Information
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Agency: Department of Defense |
Branch: Army |
Award ID: 92117 |
Program Year/Program: 2009 / SBIR |
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Agency Tracking Number: A092-020-0931 |
Solicitation Year: N/A |
Solicitation Topic Code: N/A |
Solicitation Number: N/A |