Performed FAA certified static stress and Fatigue and Damage Tolerance (FDT) analysis for retrofit antenna installationsUtilized MMPDS and NASGRO to perform fatigue and damage tolerance analysis for various airframes, including Boeing 757-300, 737-900ER and 737-800 aircraftAssessed Fatigue and Damage Tolerance scenarios to determine aircraft inspection thresholds and intervals for installed structures on Boeing 757-300 aircraft for presentation to Federal Aviation Administration (FAA)… Show more Performed FAA certified static stress and Fatigue and Damage Tolerance (FDT) analysis for retrofit antenna installationsUtilized MMPDS and NASGRO to perform fatigue and damage tolerance analysis for various airframes, including Boeing 757-300, 737-900ER and 737-800 aircraftAssessed Fatigue and Damage Tolerance scenarios to determine aircraft inspection thresholds and intervals for installed structures on Boeing 757-300 aircraft for presentation to Federal Aviation Administration (FAA) Designated Engineering Representatives (DER’s) for approval on the Supplemental Type Certification (STC) Provided onsite customer support during a prototype installation on a Boeing 737-900ER aircraft, supervising the installation and state of the structure in addition to performing onsite analysis for deviations which were submitted to the supervising DERExtensive experience developing airframe fuselage loads and stresses via classical and OEM methods to substantiate STC installationsPerformed trade studies for new radome designs and installations using FEMAP with NX NASTRAN, involving rapidly applying geometric mesh to new part designs, re-assembling the global finite element model (GFEM), and performing inertial, thermal, and aerodynamic loading stress analyses Developed compressible flow aerodynamic models in Ansys FLUENT using the Spalart-Allmaras turbulence model to determine lift and drag loads on external aerodynamic surfaces Assisted with aftermarket support of Viasat STC’s in case of damage or discrepancies noted on aircraft during flight or production installation Show less

Developed a longitudinal skin stress spectrum for Boeing 737-800 and Airbus A321 aircraft using MATLAB and FAA data to perform fatigue and damage tolerance analysis to compare with single cycle per flight FDT analysisPerformed rogue flaw and multi-site damage analysis using NASGRO, inputting both the stress spectrum and single cycle per flight stresses for hoop and longitudinal loading cases to determine inspection lifetimes

o Led the design, manufacturing, and testing of aluminum pressure vessels for LOx-Ethanol liquid bipropellant rocketo Developed heat transfer model of the liquid oxygen tank system in order to determine additional tankage needed to adjust for boiloff, calculate additional insulation sizing, and asses mitigation strategies to keep critical fluid components from getting too cold Currently developing a test plan to verify model with thermocouple temperature measuremento Performed… Show more o Led the design, manufacturing, and testing of aluminum pressure vessels for LOx-Ethanol liquid bipropellant rocketo Developed heat transfer model of the liquid oxygen tank system in order to determine additional tankage needed to adjust for boiloff, calculate additional insulation sizing, and asses mitigation strategies to keep critical fluid components from getting too cold Currently developing a test plan to verify model with thermocouple temperature measuremento Performed fatigue analysis of student designed pressure vessels to determine maximum number of safe cycles, as well as fracture analysis to determine maximum allowable flaw sizeo Led the manufacturing of propellant tank hardware such as an integral fluid diffuser and structural stringer attachment pointso Designed propellant tank with hemispherical caps, selecting tank geometry that could deliver the required impulse to the engine while being able to withstand the buckling, axial, and bending loads experienced during flight o Led the propellant tank acceptance testing campaign, performing hydrostatic tests, cryogenic cold flows, and static fires to proof and validate pressure vessel design. Improved club professionalism by integrating Military specifications into the standard operating procedures for pressure vessel acceptance testing Show less

- Performed Time Impact Analysis (TIA) on construction schedules to identify and report schedule delays- Wrote schedule update reviews to report on progress update and analyze changes in critical path - Estimated prices for construction of HVAC, plumbing, steel, and electrical components of a stadium construction project by performing takeoffs and calculating labor and material costs with RSMeans

Responsible for bagging groceries, sweeping the sales floor, and assisting customers