Development of Geometry Kernel for Dynamic Simulations

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9101-18-P-0046
Agency Tracking Number: F181-015-0442
Amount: $149,898.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: AF181-015
Solicitation Number: 2018.1
Timeline
Solicitation Year: 2018
Award Year: 2018
Award Start Date (Proposal Award Date): 2018-06-28
Award End Date (Contract End Date): 2019-06-28
Small Business Information
701 McMillian Way NW, Huntsville, AL, 35806
DUNS: 185169620
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 H.Q. Yang
 (256) 726-4800
 proposals-contracts@cfdrc.com
Business Contact
 Tanu Singhal
Phone: (256) 726-4924
Email: tanu.singhal@cfdrc.com
Research Institution
N/A
Abstract
CFDRC proposes to develop a DoD open source geometry kernel and associated APIs that can be incorporated into DoD High-Performance Computing frameworks to enable dynamic simulations of a) surface deformation or relative motion encountered in 6DOF motion of control surfaces, moving rotors in turbomachinery, store separation, and aeroelasticity; b) adaptive mesh refinement near curved boundaries; and c) use of high-order CFD solvers with curved elements. Phase I will focus on the development of a geometry kernel for improving the original linear surface mesh using three modern technologies: 1) high-order analytical NURBS fitting; 2) Bzier surface fitting, and 3)modern subdivision surfaces, which has been widely used in computer animation and video games. The Phase I effort also includes curved surface element generation using the high-order NURBS analytical surface; coupling to the volumetric mesh deformation to improve the quality of curved meshes; and demonstrations for the problems of a) moving body, b) aeroelasticity and c) high-order element generation. Phase II will establish a versatile set of APIs comprising a well-developed geometry kernel to efficiently perform commonly required tasks related to geometry and associated computational meshes, and the source code will be provided for incorporation into larger DoD developed tools and frameworks.

* Information listed above is at the time of submission. *

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