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High Temperature Fracture Mechanics

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0860-20-C-7057
Agency Tracking Number: B19C-002-0040
Amount: $99,973.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: MDA19-T002
Solicitation Number: 19.C
Timeline
Solicitation Year: 2019
Award Year: 2020
Award Start Date (Proposal Award Date): 2020-04-06
Award End Date (Contract End Date): 2020-10-05
Small Business Information
700 N. Brand Blvd. Suite 700
Glendale, CA 91203
United States
DUNS: 055775803
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Joe Magallanes
 CEO/Principal
 (818) 240-1919
 magallanes@kcse.com
Business Contact
 Joseph Abraham
Phone: (818) 240-1919
Email: abraham@kcse.com
Research Institution
 Penn State University
 Mike Hillman Mike Hillman
 
Civil and Environmental Engineering 224A Sackett Building
State College, PA 16801
United States

 (814) 863-0623
 Nonprofit college or university
Abstract

This STTR research study aims to enhance and apply thermo-mechanically coupled computational models for high-temperature fracture. This topic is particularly challenging in that hypersonic flight in the atmosphere generates extreme conditions over a vehicle that can affect the strength and performance the vehicle materials, both in-flight conditions as well as for cases where the vehicle encounters projectile impacts. To address this highly challenging problem, K&C and PSU have the unique expertise and capabilities of enhancing state-of-the-art thermo-mechanically coupled Computational Solid Dynamics (CSD) and Computational Fluid Dynamics (CFD) models that are required to understand the interaction of the high-temperature environment with the fracture associated with hypersonic vehicles. The Phase I seeks to research and extend coupled CSD/CFD codes to model the perforation of a vehicle, the resulting dynamically evolving flow-field through the opening, while retaining the essential coupling phenomenon. K&C’s existing thermo-mechanical material model for Ceramix Matrix Composites (CMCs) will be extended and calibrated to existing and new data. Armed with an increased computational capability to model thermo-mechanical coupling phenomenon with hypervelocity materials, we propose to conduct a limited suite of coupled CSD/CFD hypervelocity calculations under flight conditions (Mach 5) and under transient impact with projectiles. Approved for Public Release | 20-MDA-10398 (2 Mar 20)

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

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