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Additional Engineering Resume Samples
Stress Engineer Resume Samples
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6-10 years of experience
Built and trained 8-person team of new engineers on structural analysis of highly specialized missile handling equipment. Created training materials for entry-level engineers.
- Developed each team member into self-sufficiency within three months and many were identified for promotions in six months.
- Streamlined on-board training process for new engineers.
- Promoted twice based on outstanding performance recognized by customers and upper management.
0-5 years of experience
Analyzed stress in aircraft components using Excel and FEMAP with NASTRAN Finite Element Modeling.
- Wrote official stress reports explaining part sizing, analysis methodology and compliance for customer review.
- Investigated areas for improved efficiency and provided customer liaison services in Switzerland for 6 months.
- Created stress analysis spreadsheets for electrical brackets on a fast-paced project in Spain for 7 weeks.
6-10 years of experience
Performed stress analysis by using hand calculations and finite element method (FEMAP& NASTRAN).
- Documented structural substantiation reports to meet 14 CFR Parts 23 and 25 regulations.
- Provided design guideline, structural test support and MRB repairs to ensure the airworthiness of aircraft structural modifications.
- Evaluated engineering drawings, design concept and material/parts selection to meet structural integrity.
0-5 years of experience
[company name] provided the design and stress analysis of various interior components of VIP aircraft. Certification of the aircraft was provided at project completion.
- Led team of 3 engineers for stress analysis, providing status updates to management and customer.
- Wrote substantiation reports for aircraft submitted to Federal Aviation Administration (FAA) and European Aviation Safety Agency (EASA) approval standards.
- Sent to off-site designated engineer representative’s company for liaison services, provided analysis and customer support during 3 month assignment which reduced number of reports requiring completion by 90% in constrained timeline.
0-5 years of experience
Substantiated Wing to Body fairing access door modification using classical laminate theory (CLT) and FeMap/NX Nastran v4.1 to obtain STC. Analysis included layer by layer stress analysis using Tsai-Wu failure criterion, Eigen value stability check, fastener loads, boundary condition substantiation, sensitivity runs, repair doubler design, and load path optimization.
- Created fuselage access panel hole modification report with stability analysis per shear buckling criterion and ring doubler design with analysis based on equivalent strength.
- Produced a pull-out table analysis report. Performed load path analysis, static equilibrium calculations, and evaluated integral vs. built-up beam concepts for the abuse load case.
- Developed A and B basis insert allowables in shear and tension for MidCoast composite honeycomb panels. Testing was performed per ASTM standards.
0-5 years of experience
Worked on a jet avionics structure cabinet to check structure adequacy during flight load cases.
- Contributed to the design and analysis of Radar Antenna structures to withstand high wind loads.
- Analysis involved heavy classical hand calculations and CAE analysis using Patran and Nastran.
- Wrote formal stress reports to comply with FAA and Military requirements.
0-5 years of experience
Assessed diverse failure modes on multiple components of the exhaust system for the Bombardier C-Series, Boeing 787 Dreamliner, Mitsubishi Regional Jet, and Airbus A350 and A320 programs.
- Altered finite element models and conducted finite element analysis to support the stress analysis needs on various exhaust components.
- Aided in ensuring on time completion of preliminary design reviews, critical design reviews, flight readiness reviews, and means of compliance reviews.
- Performed stress analysis on metals under extreme conditions, including methods for low cycle fatigue analysis, high cycle fatigue analysis, static strength check (using limit loads, ultimate loads, and fan blade off loads).
- Developed VBA macros to read and process results into usable data
0-5 years of experience
Led the team in design and problem solving; coordinated multiple projects
- Participated in more than 10 projects, including commercial building, shopping and business centers
- Reduced material cost by conducting risk mitigation on structure under wind and seismic hazards
- Collaborated with developers and clients to research and designed building structures
- Advanced structure safety through commercial software, evaluated and mitigated emergency and resolved technical problems on site
0-5 years of experience
Performed finite element stress analysis of composite panels in aircraft flooring using Patran & Nastran
- Estimated initial sizing of the panels using classical methods. Calculated preliminary skin stress, core shear stress
- Defined load paths, panel type, optimum skin thickness. Developed a FEA model in Patran & Nastran for validation
- Documented test plans with test results & final design for DGCA-India certification under FAA regulations
0-5 years of experience
Engine Nacelles / Analysis Standards AIRBUS A350 XWB
- Responsible for preparing and integrating technical presentations for internal/external design reviews
- Appointed as the Goodrich Subject Matter Expert and A350 XWB POC for composite panel joint analysis
- Performed and documented static and fatigue analysis for metallic and composite nacelle components
- Programmed Excel Visual Basic and Access based standard analytical tools for company-wide use
0-5 years of experience
Developed internal loads Finite Element Models (FEM) for ultimate, fatigue, and damage tolerance analysis on the Boeing 737 airplane.
- Helped develop fine mesh FEM for analysis of high stress regions of an airplane.
- Post-processed data for use in classical stress analysis.
- Performed classical hand stress analysis.
- Verified commercial airline internal load FEMs conversions from CATIA-ELFINI to NASTRAN.
- Worked on development of tools to post-process NASTRAN data to be used with internal company software.
- Served as a summer intern mentor in the summers of 2007, 2009, and 2010 which included teaching and modeling good engineering practices and helping them with daily life tasks in Wichita, KS.
0-5 years of experience
Led a team in structure design and problem solving following design codes
- Performed static/dynamic stress analysis of large scale structures using ABAQUS, linear modal analysis of steel structures using ANSYS
- Optimized design with material cost/budget subjected to risk assessment on structure under wind and seismic hazards
- Participated in more than 10 projects, including commercial building, shopping and business centers
- Advanced structure safety through commercial software, evaluated and mitigated emergency and resolved technical problems on site
0-5 years of experience
Helped set up foundation of in-country Stress Analysis group.
- Established Stress Analysis Guidelines for in-county engineers.
- Supported major layout of load-path structures for entire T-50 airframe.
- Led training lectures and daily mentored in-country engineers.
- Supported detail design of center fuselage structure for T-50 airframe.
- Assisted the Korean lead of the Center Fuselage Stress Analysis group.
0-5 years of experience
- Performed stress analysis to calculate forces, vibrations, thermal expansion within complex piping systems for power and process applications using CAESAR 5.0
- Analyzed piping layouts to specify the different load supports to be applied on the cross-sections of the pipes.
- Designed the specifications and performed product testing of pipes and other piping related components based on standard ASME 31.3.
- Prepared and verified the specifications for various mechanical components such as pumps, motors, compressors.
- Created pipe layout and isometric drawings with the data from process, instrumentation and mechanical departments.
- Assisted with preparation of Piping – Instrumentation diagrams and line list to ensure seamless development efforts
0-5 years of experience
Lead engineer over 5 other engineers on the Cessna Citation Bravo thrust reverser project
- Analyzed the nozzle assembly , doors , and actuators , on the Cessna Excel thrust reverser project
- Performed a great deal of composite analysis and testing. Wrote test plans and reports for tension , compression , and beam tests
- Stress and fatigue analysis on hush kits for 737 engines
- Used ANSYS to model and analyze thrust reverser parts where the complexity of the part demanded it
- Automated all of my analysis using Mathcad and Excel so that the effects of changing loads or other parameters could be examined very quickly
6-10 years of experience
Performed flight deck seat track analysis (CATIA-V4, Catia-Elfini & Hand analysis), prepared analysis report / strength check notes, drove improvement of the test procedures, and coordinated additional testing requirements with the vendor
- Developed 16G dynamic and 9G static flight test requirements, procedures, instrumentation and configuration definition
- Reviewed and approved structural test plans and reports (for improvements, thoroughness, and clarity) for FAA/FAR (Federal Acquisition Regulations) certification of seats, lavatories, galleys, space integrated carts, electrical payloads equipment and other payloads commodities
- Led our engineers in the development of standard test methods and processes; and applied advanced test technologies to develop test procedures. Emphasis was on proper test setup, minimizing risk, verification of test methods, and procedural content to meet FAA/FAR, customer, and [company name] requirements
- Coached, managed and trained overseas [company name] Development Center (BDC) engineering team in the development of seat interface loads (via Proprietary “SeatLoads” Program). Collaborated with BDC management
- Maintained proprietary software program that runs an Excel based Visual Basic application used for generating structural interface loads for aircraft seats to meet formatting and content requirements of the customer
0-5 years of experience
St. Lucie Nuclear Power Plant (FPL)Extended Power Uprate Project
- Analyzed ASME Class 2 & 3 and B31.1 Piping Systems.
- Prepared and Checked Pipe Stress Calculations
- Performed Design Verification
- Calculations: (i.e. Qualified Penetrations, Wall Thickness, IWA’s, etc.)
- Reviewed P&ID’s and Initiated Engineering Changes
- Performed Walk Downs
0-5 years of experience
Support in GAMESA 4.5 MW wind turbine calculations in the Design Department
- Working as part of the Mechanical Engineering Design department of GAMESA
- Development of FEA (PATRAN/ABAQUS 6.8) for different parts of the 4.5 MW wind turbine, having as input CATIA design files at different design stages
- Organization and interpretation of large amount of electronic data resulting from Finite Element Analyses
- My final interpretations of the analyses led to the refinement of the design in the next design steps of the design iteration process for the analyzed structural parts
0-5 years of experience
Completed static and dynamic stress analysis of piping systems in support of The Department of Energy’s (DOE) Salt Waste Processing Facility (SWPF) located at the Savannah River Site in Jackson, SC. in accordance with ASME, ANSI B31.3 code requirements using Caesar II software program.
- Used loads obtained from Caesar II to qualify tank and pump nozzle allowable loads provided from vendor.
- Verified supports dimension and location using Smart Plant
- Coordinated with lead to improve documentation procedure to ensure documents and calcs are updated and can be tracked easily.
- Delegated work assignments and maintain work schedule. Manpower allocation
0-5 years of experience
Perform Pipe stress analysis as per the input data (geometry, load cases) using CAESAR II specific application of static and dynamic analysis for seismic load conditions. Checked complete pipe stress package, type of support & analyzed loads including nozzle. Modeled support components per stress analysis for standard and engineered supports.
- Prepared support drawings showing detail such as dimension, weld, bill of material and notes for engineered support to prepared calculation and update ISO drawings for construction.
- Evaluate all piping supports, restraints and anchor loading are maintained within an acceptable range and the flanged and mechanical joint have been evaluated for leakage as defined by ASME Section III, Division 1, NC-3658 and ASME B16.
- Checked plant layout, P&ID, PFD, piping isometrics, piping/equipment specifications, piping bill of material, data sheets and with good experience in piping sizing and thickness calculations.
- Involved in assembling bid packages for piping purchase inquiries to be issued for procurement of materials or subcontract pricing, technical evaluation of all piping bids
- Attained troubleshooting in piping turnaround and construction fabrication modification activities.
0-5 years of experience
Coordinated all Stress Analysis Work
- Performed stress analysis using computational and analytical methods
- Approved all design details from Design Graphics
- Handled job site issues with site visits
- Ensured design teams followed and applied all required codes for design of Selective Catalyst Reduction (SCR) and WFGD/DFGD (Wet/Dry Flue Gas Duct) systems using ASME, ASIC, AWS, KBC, UBC, etc.
6-10 years of experience
- Led technical team to deliver structural analysis ahead of schedule and to specification
- Collaborated with multidisciplinary team to schedule technical tasks using MS Project
- Presented analysis to internal and external customers at five technical design reviews
- Developed analysis tools to certify aerospace components with airworthiness authorities
- Performed static, fatigue and damage tolerance analysis on titanium aerospace components
- Authored technical documents describing aforementioned analysis tools and methods
6-10 years of experience
- Performed detail FEA on several interior monuments using Elfini and also hand calculations to meet structural integrity requirements.
- Reviewed and edited 2D engineering drawings of internal structures.
- Supported certification testing team in static test plans to determine strength of different fiber composite materials, inserts and panel pins.
- Developed and documented structural analysis substantiation reports for FAA and EASA certification of Falcon 2000, 900 & 7X aircrafts per FAR part25.
- Assisted design & production departments to substantiate damages and repairs on interiors and primary aircraft structures.
- Supported offsite vendors (Dassault Systemes & Mahindra Satyam) for review and completion of FEA.
- Coordination with Dassault Aviation in generation of interface loads reports for the basic aircrafts.
- Provided continuous support to CATIA DAV tools department in improving Excel macros for Elfini, which in turn reduced pre & post processing time to perform FEA and generation of report by 35%.
- Other analysis performed:-rigid body analysis, damage tolerance analysis, decompression analysis, reinforced floor board analysis, fatigue analysis.
0-5 years of experience
On-site stress analysis supporting Boeing 787-8 and 787-9 programs.
- Performed structural optimization trade studies for metal and composite parts and led other Boeing engineers in support of 787-9 program.
- Performed static and fatigue analysis and led other Boeing engineers in support of 787-8 certification.
- Learned metallic and composite optimization techniques using Altair Optistruct through company sponsored training.
0-5 years of experience
Analyzed new product metal and composite strut structures for damage tolerance and static strength capability.
- Prepared analyses for FAA Type Certification.
- Developed and analyzed flight capability and maintenance manual inspection requirements for aircraft experiencing engine fan blade out damage and subsequent windmilling events.
- Analyzed and prepared structural inspection data documentation for Airline Customer Certification Compliance to FAA and JAA.
0-5 years of experience
- Analyzed and interpreted engineering drawings and data
- Evaluated impact of increased static and flight loading conditions on proposed aircraft
- Calculated load exceedance and reserve factors (LEFs and RFs) on various wingbox rib components
- Located critical and underperforming elements for further monitoring and analysis
- Composed static stress analysis documents
- Re-examined documents to maintain quality control standards
- Utilized client proprietary software to meet customer requirements
0-5 years of experience
- Performed strength and stability analysis of aircraft primary and secondary structures.
- Prepared stress and strength analysis substantiation reports of aircraft structure components based computer analysis and hand calculations.
- Conducted finite element modeling and analysis (FEA) of aircraft installations using FEMAP with NASTRAN.
- Reviewed and released structural design drawings based on strength validation.
0-5 years of experience
Carried out stress analysis of Guide and Restraint Systems of A400M Military Cargo Handling Systems using classical hand calculations
- Knowledge of AIRBUS stress calculation methodologies
- Prepared stress analysis reports of Cargo Handling System Components as per FAA and EASA requirements
- Coordinated with AIRBUS engineers to resolve various issues related to analysis/certifications
0-5 years of experience
Performed detailed stress analysis for engine and nacelle latching systems (hand calcs, Mathcad).
- Performed non-linear FEA (MSC Nastran Sol106) where needed (Material & Geometrical non-linearity).
- Prepared test and qualification plans (CTP’s & QTP’s).
- Performed test correlation analysis.
Gabriela Barcenas
CPRW, Content Writer IIGabriela is a Certified Professional Resume Writer (CPRW) and career adviser. With 10 years of digital media experience and five years of resume writing expertise, her publication history includes fashion, education, travel, social justice, equitable design and career advice.
