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Multi-Physics Models for Parachute Deployment and Braking

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9550-18-P-0020
Agency Tracking Number: F18A-004-0035
Amount: $149,999.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: AF18A-T004
Solicitation Number: 18.A
Timeline
Solicitation Year: 2018
Award Year: 2018
Award Start Date (Proposal Award Date): 2018-09-15
Award End Date (Contract End Date): 2018-09-15
Small Business Information
566 Glenbrook Drive
Palo Alto, CA 94306
United States
DUNS: 172390481
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Goeric Daeninck
 Senior Research Scientist
 (650) 530-2435
 gdaeninck@cmsoftinc.com
Business Contact
 Frankie Farhat
Phone: (650) 898-9585
Email: ffarhat@cmsoftinc.com
Research Institution
 Virginia Tech
 Kevin Wang Kevin Wang
 
Kevin T. Crofton Department of Aerospace and Ocean Engineering Randolph Hall Rm. 332-3
Blacksburg, CA 24061
United States

 (650) 862-2663
 Nonprofit college or university
Abstract

The main objective of this STTR Phase I effort is two-fold. First, to develop a robust approach for coupling the flow solver Kestrel with the multidisciplinary software tool AERO Suite in order to enable the physics-based modeling and simulation of the dynamics of Aerodynamics Decelerator Systems (ADS) such as parachutes from deployment to terminal velocity or terminal descent and touchdown, and the effect of such ADS on bodies of interest. Second, to demonstrate its feasibility. The key components of this approach are a Chimera-based overlapping domain decomposition method for coupling Kestrel and AERO-F in space, and a stable and second-order flexible procedure for coupling them in time. The key enablers of the resulting simulation capability are the following pillars of AERO Suite for the simulation of highly nonlinear fluid-structure interaction problems: the second-order embedded boundary method FIVER (Finite Volume method with Exact two-material Riemann problems) for achieving robustness with respect to large structural motions and deformations, self-contact, and topological changes; the associated adaptive mesh refinement module for tracking boundary layers, shocks, and other flow features and keeping them at all times well resolved; and the corresponding dynamic load balancing strategy for achieving acceptable parallel performance on DoD HPCMP architectures.

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

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