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Aerothermoelastic Simulation

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9302-08-M-0009
Agency Tracking Number: F073-145-0426
Amount: $99,965.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: AF073-145
Solicitation Number: 2007.3
Timeline
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-03-12
Award End Date (Contract End Date): 2008-12-08
Small Business Information
566 Glenbrook Drive
Palo Alto, CA 94306
United States
DUNS: 172390481
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Goeric Daeninck
 Research Scientist
 (650) 941-4301
 gdaeninck@cmsoftinc.com
Business Contact
 Charbel Farhat
Title: President
Phone: (650) 353-0540
Email: cfarhat@cmsoftinc.com
Research Institution
N/A
Abstract

Hypersonic flight introduces extreme heat loads into the skin of a vehicle, particularly at its leading edges. Determining these loads is a challenging task that requires accounting for the aerothermal features of both the flow and thermal state of the surface of the structure. Hence, the accurate aerothermal analysis of hot vehicles requires a tight coupling between appropriate fluid, thermal, and structural models. Incomplete forms of this integration have been attempted in the past using simple algorithms that were either computationally inefficient or numerically unstable. The main objectives of this proposal are: (a) to demonstrate a higher-fidelity, multidisciplinary computational technology for the analysis of hot vehicles that is numerically stable, provably accurate and compatible with the AERO code deployed at the Edwards AFB, and (b) equip this simulation technology with a reliable Reduced-Order Modeling (ROM) capability to enable the prediction in near real-time of heat loads and their effects on structural integrity and aeroelastic stability. The proposed high-fidelity approach centers on the four-field formulation of aerothermoelastic problems and provably accurate and computationally efficient conjugate heat transfer algorithms for deformable and vibrating structures. The proposed ROM technology is based on the Proper Orthogonal Decomposition (POD) method.

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

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