Khari Harrison

ORCID: 0000-0003-2464-644X
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About
Contact & Profiles
Research Areas
  • High-Velocity Impact and Material Behavior
  • Transportation Safety and Impact Analysis
  • Mechanical Behavior of Composites
  • Structural Response to Dynamic Loads
  • Electrical Fault Detection and Protection
  • Icing and De-icing Technologies
  • Material Properties and Processing
  • Engineering and Material Science Research
  • Polymer crystallization and properties
  • Lightning and Electromagnetic Phenomena
  • Laser-Plasma Interactions and Diagnostics
  • Fiber-reinforced polymer composites
  • Electromagnetic Launch and Propulsion Technology

Texas A&M University
2021-2024

Walker (United States)
2021-2024

Mitchell Institute
2021

Novel engineering materials and structures are increasingly designed for use in severe environments involving extreme transient variations temperature loading rates, chemically reactive flows, other conditions. The Texas A&M University Hypervelocity Impact Laboratory (HVIL) enables unique ultrahigh-rate characterization, testing, modeling capabilities by tightly integrating expertise high-rate behavior, computational polymer chemistry, multi-physics multiscale numerical algorithm...

10.1063/5.0088994 article EN publisher-specific-oa Review of Scientific Instruments 2022-08-01

When developing protective structures to defend against hypervelocity impacts (HVIs), optimizing specific energy dissipation is critical. Incorporation of lightweight materials, such as polymers, into novel layered shielding concepts could improve HVI performance in space and military applications without compromising cost or weight. One key challenge a fundamental understanding the effects molecular architecture on macroscopic dynamic material response damage formation. In this work, two...

10.2514/6.2021-0887 article EN AIAA SCITECH 2022 Forum 2021-01-04

In this study, hypervelocity impact experiments were performed on both unstitched and through-thickness Vectran™-stitched laminates. Both laminate types fabricated from DMS-2436 class-72 warp-knit multiaxial carbon fabric, infused with API-1078 resin using a Controlled Atmospheric Pressure Resin Infusion (CAPRI) process. The laminates impacted by 4 mm diameter, spherical, Nylon 6/6 projectiles at nominal velocities of km/s two-stage light gas gun. primary measures the performance composite...

10.12783/asc36/35800 article EN American Society for Composites 2022 2021-09-20

In-flight lightning strike damage to aircraft composite structures may compromise airworthiness. Hence, it is crucial incorporate adequate protection systems mitigate the current. Most (LSP) techniques involve bonding a metallic conductive layer cured laminate exterior. In this study, novel LSP integration technique was used develop unitized panels with three different layers: pitch carbon fiber paper (PCFP), graphene (GP), and copper mesh (CM). Each overlaid on through-the-thickness...

10.12783/asc36/35743 article EN American Society for Composites 2022 2021-09-20
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