Engineering Commons^™

Landing-Gear Impact Response: A Non-Linear Finite Element Approach, Tuan H. Tran

UNF Graduate Theses and Dissertations

The primary objective of this research is to formulate a methodology of assessing the maximum impact loading condition that will incur onto an aircraft’s landing gear system via Finite Element Analysis (FEA) and appropriately determining its corresponding structural and impact responses to minimize potential design failures during hard landing (abnormal impact) and shock absorption testing. Both static and dynamic loading condition were closely analyzed, compared, and derived through the Federal Aviation Administration’s (FAA) airworthiness regulations and empirical testing data.

In this research, a nonlinear transient dynamic analysis is developed and established via NASTRAN advanced nonlinear finite element model (FEM) to …

A Process, Structure, And Property Study Of Gallium-Based Room Temperature Metallic Alloys, Courtney Lyn Titus

UNF Graduate Theses and Dissertations

Amalgamations are a promising replacement for electronic solders, thermal interface materials, and other conductive joining materials. Amalgams are mechanically alloyed materials of a liquid constituent with a solid powder. Unlike traditional solders, these materials are processed at room temperature or slightly above, and can often operate at temperatures near, or beyond, their processing temperatures. Existing bonding processes require an excessive amount of heat, which may cause thermal stress to the electronic components and delaminate the attachment. Amalgams have promising characteristics for thermal interface materials (TIMs) due to being fully metallic, relatively easy of handling, and possessing metallic strength similar to …