skills required.doc

7/28/2019 skills required.doc

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Aeronautical jobs

Structural analysis

Experience in finite element modeling and analysis using Ansys/ Nastran/ Patran/Hypermesh/ LS Dyna and Abaqus. Candidates should have hands-on experiencewith various analysis types such as linear statics, non- linear statics (contact,material and large deformation), dynamics, etc. Expertise in 2D/3D FE modeling foraero-engine/ turbo Machinery / automotive /heavy engineering components ispreferred. Experience in interpreting and understanding FEA results, post-processing and preparing comprehensive analysis reports.

Experience in Aircraft structures, preferably in any one of the following areas:Analysis of Primary & Secondary (Fuselage, Wing, Empennage) structures.Knowledge andhands-on experience in Stress analysis (Composite & Metallic) and to check thedetailed stress analysis as per any OEM standards. Knowledge and hands-onexperience in Fatigue & Damage

Tolerance analysis (Composite & Metallic). Working knowledge of Patran/NastranandExcel VBA will be preferred.

Hands on experience in FE modeling of composite and metallic structuresProficient in NASTRAN & PATRANProficient in structural analysis (linear and non-linear methods)Standard Hand Calculation methods for primary and secondary componentsStrong in fundamentals and basics of EngineeringGood knowledge in excel macros and stress dossier preparation

Knowledge on Aircraft loads

Experience in Fatigue and Damage Tolerance analysis - Spectrum generation,life cycle estimation of Aircraft components, Crack propagation studies

Experience in Patran/Hypermesh and Nastran is a must

Must have exposure to tools such as SAFE, ISSY, ISAMI- static and F&DTmodules

Preparation of certification documents

Preparation of compliance report FAA regulations


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Aerospace domain(aero structures, aero engines and/or wind turbines)Stress Analysis(including finite element modeling)Fatigue & Damage ToleranceComposite Materialswill be preferred.

Ideal candidate for this position should be conversant with latest analysistools & industrial analysis methods & standards

Experience in stress analysis of Aero structures

Exp in Composites is mandate

Performs structural analysis of a complex nature using conventional hand analysis and/computer analysis

Establish, develop and validate structural design concepts of nacelle components throughstatic and dynamic assessment of metallic and advanced composite aero-structures andnacelle components using semi-empirical and analytical approaches.

Experience in aerospace industry, with some design and structural stress analysisexperience, preferably with airframe structures

Good in hand calculation and nastran and patran tools.

Analyze and provide design solutions for the structural integrity of advancedcomposite aircraft interior structures using classical methods and advanced

Finite Element Analysis.Develop enhanced capability in the area of composite analysis

Analysis of aircraft wing structures preferably trailing edge components Familiarity with the aircraft wing loading

Exposure to product life cycle from design to certification, in-service and failureinvestigation


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Use of ISAMI for Fatigue requirements

FE modeling and analysis skills using Hypermesh/Nastran/Patran

1. Perform 3D FEM

2. Understand and work on Hex and Tet10 elements

3. Perform FEA on large integrated assembly

4. Aerospace related hand calculations

5. FEA relating to Composites including pcomps

6. Structural analysis on Metallics

7. Work on NASTRAN and PATRAN softwares

8. Undertstand Composites / laminate theory

9. Formulate and implement finite element stress analysis (FEA) plans to achieve technicalrequirements, schedules and program commitments

Post Graduate/Bachelor of Engineering in Aeronotical / Mechanical background.

3-10 years of experience in Stress Analysis

Hands on experience with MSC Software like NASTRAN and PATRAN.

Excellent knowledge of stress analysis using FEA, hand calculations or spreadsheet basedtools.

Experience of Check stress, Airbus internal tool and hand calculations usingBruhn/Niu/Roark/Peterson framework

Good knowledge of 3D linear and non-linear, single or multi time point, steady-state andtransient analysis

Knowledge on iFEM, comfortable with large integrate assembly FEA

Hands on experience with Composites FEA

Working knowledge with Structural Analysis

Ability to work in a global environment.

Knowledge on preparing technical reports after the completion of the project.

Fluency in English.

Must be ambitious, like to work hard, be highly motivated, and able to work in a fast- paced environment


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Must demostrate highest standards of integrity reflected in all external and internalcommunications

Exceptional communicator in written, graphical and oral forms, with a collaborative andflexible style.

Self-motivated, high energy, respectful, honest, hard-working and loyal team player.

Analyze and provide design solutions for the structural integrity of advancedcomposite aircraft interior structures using classical methods and advancedFinite Element Analysis. Develop enhanced capability in the area of composite analysis

Static&Non linear Analysis of Aircraft structures, linear Analysis involved inthe analysis of structures using a broad range of standard hand&computermethods(eg. Nastran&Patran).Min 7+yrs exp in Aero structures&stressanalysis,hand calculations/FEM

To become part of Aircraft Engine Product Engineering Center team by executingstructural stress analysis programs with strict adherence to quality and timelinecommitments.

The broad responsibilities are as follows:-Lead and Execute static/rotating parts certification, life extension and design analysis

programs across engine lines.-Provide engineering analysis support for improving design and for manufacturing /supplier / field issues-Ensure on-time delivery with FTY=1 adhering to Toll gate review process-Effectively communicate and Collaborate with different groups at global sites and

execute program plans-Demonstrate in-depth technical expertise at a system/domain/program level-Mentor team members on project execution-Participate in stress analysis process improvements and work towards ownership of stress analysis best practices- Life Methodologies

The incumbent would be a part of the Landing Gears division at the India DesignCenter facility in Bangalore.

Involved in Structural Analysis using hand calculations (classical methods),ABAQUS FEA software and in-house codes / tools.

Closely interact with the concerned Leads, communicate regularly with the customer,understand their needs, develop plans, take full ownership of projects and drive them toclosure.

Meticulously conduct self-quality checks of the deliverables and ensure they meetcustomer requirements / standards.

Strong knowledge of mechanical engineering fundamentals / principles.


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Strong background in performing stress analysis using hand calculations (classicalmethods) and ABAQUS FEA software.

Ability to work well either individually or in a team.

Excellent communication and problem solving skills.

Familiarity with mechanical aircraft components and systems.

Exp in Landing gear systems is preferred

Analyse and provide design solutions for the structural integrity of advanced compositeaircraft interior structures using classical methods and advanced Finite Element Analysisusing ANSYS and some good knowledge on Nastran

Excellent expertise in application of engineering principles and theories in structuralanalysis and test methods.

Experience in composite structural analysis Strong knowledge of mechanical engineering fundamentals / principles.

Strong background in performing stress analysis using hand calculations(classical methods) and ABAQUS FEA software.

Familiarity with mechanical aircraft components and systems.

Involved in Structural Analysis using hand calculations (classical methods),ABAQUS FEA software and in-house codes / tools.

-B.Tech/ME with Aerospace Engineering with around 5-10 years of experiencein Aircraft Structures-Expert in Airframe Stress Analysis using FEA (Mandatory) and ClassicalPrinciples-Experience in Weight Optimization /Sizing procedures of Primary AircraftStructural components-Should be able to offer alternate design/analysis methodologies based onthe requirement-Should have strong hands on experience with Nastran/Patran/Hypermeshand CATIA (Mandatory)-Clear understanding of Aircraft Components and their functions is required.-Prior Experience with Bombardier or any OEM Stress/Optmization proceduresis an added

Should have exposure of Aerospace Domain and Airbus Projects.Candidate should b willing to travelShould have worked on Nastran, Patran , ISMAI,Hypermesh

* You have a strong knowledge in metallic materials and manufacturing processes.* You have good experience in Finite Element Modeling using PATRAN / NASTRAN tosupport design activities


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Establish, develop and validate structural design concepts of nacelle components through staticand dynamic assessment of metallic and advanced composite aero-structures and nacellecomponents using semi-empirical and analytical approaches.

Experience in aerospace industry, with some design and structural stress analysis experience, preferably with airframe structures

Good in hand calculation and nastran and patran tools.

Bachelor / Master of Engineering in Mechanical / Aerospace Engineering with 2 - 12 Years of experience in Airframe Stress analysis

v Strong fundamentals in strength of materialsv Hands on Experience in the analysis of primaryand secondary airframe structures using Bruhn, Niu and ESDUs v Knowledge on Bombardier methodology would be an added advantagev Working Experience in PATRAN / NASTRAN vBasic knowledge in CATIA V5

Basic Qualifications : B.E/B.Tech with 5 to 7 years of experience in Mechanical/AerospaceEngineering with expertise in structural analysis.

Knowledge and understanding of aerospace and/or automotive structural components.

Capable of performing FEA analysis for Random Vibration analysis using ANSYS Workbench.

Familiar with Fatigue Damage Evaluation.

Familiar with PCB mounted components.

Familiar with ferrous (steel & stainless steel) and non-ferrous (aluminum) casting and forgingtechniques.

Familiar with designing products to industry, agency, or military standards (can read andunderstand industry or MIL standards).

Capable of working within schedule and under stress.

Excellent writing and PC skills to prepare analysis reports and trade studies.

Strong verbal communication.

Ability to work independently with minimal supervision


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Basic Qualifications : B.E/B.Tech with 6 to 9 years of experience in Mechanical/AerospaceEngineering with expertise in structural and fluid analysis.

Knowledge and understanding of aerospace and/or automotive structural components.

Capable of performing FEA analysis using PATRAN/NASTRAN

Familiar with CFD using Ansys or Fluent; previous experience with either desired.

Familiar with fluid handling product design and seal design (greater than 1000 psi pressure).

Familiar with ferrous (steel & stainless steel) and non-ferrous (aluminum) casting and forging

techniques.

Familiar with designing products to industry, agency, or military standards (can read andunderstand. industry or MIL standards.)

Capable of working within schedule and under stress.

Excellent writing and PC skills to prepare analysis reports and trade studies.

Strong verbal communication.

We are looking for Tech Lead - Stress analysis for our aerospace Client in Bangalorelocation.

Should have Strong engineering fundamentals with 7 to 10 years of experience instress analysis using Hand calculation & FEA NASTRAN / PATRAN.Strong application of engineering principles and theories in structural analysis, loadcalculations and test methodsVery good knowledge of NASTRAN/PATRAN and Hypermesh

Experience in aerospace domain & composites materials is an added advantage

Post-Graduation in Mechanical, Automotive, Production, Aeronautical Engineering with atleast 8 Years of Automotive Analysis experience

Knowledge of computer software for crash safety applications: LS-DYNA or Radioss or HYPERWORKS or BetaCAE or PRIMER or Hypercrash


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Qualifications - Postgraduate in Mechanical/Aerospace Engineering with specializationin turbomachinery aerodynamics, computational fluid dynamics

Good knowledge of turbomachinery aerodynamics

Strong oral and written communication skills

Strong interpersonal and leadership skills

Good work ethics

Demonstrated ability to analyze and resolve problems

Ability to document, plan, market, and execute programs

Desired Characteristics -Experience in axial compressor or turbine aerodynamics design

Prefer individuals with 5+ years of relevant experience

AERODYNAMICS DATA ENGINEERAs an Aerodynamics Data Engineer aligned with Aerodynamics Data Team, themission of the jobholder will consist in contributing to the development of Airbusaerodynamics data domain processes employed for aerodynamics datageneration and analysis. To continuously improve the aerodynamics data modelsand processes throughout the aircraft development cycle.

MAIN RESPONSIBLITIES

Get a full knowledge of existing aerodynamics data models & processes To understand the methods and tools employed for the aerodynamics data

productionContribute to the delivery of the aerodynamics data deliverables (AerodynamicsCFD, Modelling)o According to the agreed work plan to time, cost and qualityo In compliance with specifications, requirements and applicable Airbus policies.Carry out the validation tasks required to meet customers needsContinuously look for the improvement for aero data modelling processes andpatent the new modelling process in compliance with the Airbus rules andpolicies

QUALIFICATIONSMasters degree in Aerospace with CFD background

SKILLS The candidate will preferably have experience or qualifications in one or acombination of thefollowing areas:

Technical Skills:Knowledge of the CFD Process (Meshing, Solvers, Post processing) & Toolsrelated to the process


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4)Development of Integrated Flow/Thermal and deflection models for Gas Turbine Applications.

5)Perform Heat Transfer and Secondary Flow Design and analysis for Commercial aircraft,Marine and Industrial Aero derivative engines for Steady state and Transient Conditions.

6)Consistent in meeting the commitments, able to handle multiple projects.

7)Should be proficient at developing presentations, summarizing conclusions/recommendations.

8)Communication and Interface with other design groups.

9)Make recommendations after analysis of the data using quality tools.

Qualifications/Requirements

1)Masters/PhDs in Thermal/Fluid Mechanics/Propulsion specialization with strong academic

track record.

2)Experience in FEA Software like Ansys, Patran and Hypermesh.

Desired Characteristics

10+ years experience in aerospace industry with Good Knowledge of Heat Transfer andCompressible Fluid Flow.

Knowledge of CFD and CFD packages like Fluent and CFX.

Demonstrated application of Creativity and innovation in solving problems.

Strong oral and written communication skills

Strong interpersonal and leadership skills

Demonstrated ability to analyze and resolve problems

Ability to document, plan, market, and execute programs

Demonstrated leadership in advancing the state of the art in a technical specialty

Perform CFD analysis of sub-system, system using available CFD tools. Interact withcustomers,

Understanding requirement , interpreting physics and giving design suggestions based onsimulation

Nature of Experience


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CFD Simulation Should have strong knowledge of fluid mechanics, heat transfer & thermal Engineering

Exposure to CFD tools like FLUENT/CFX/STAR-CCM/ACUSIM

Strong analytical and problem solving capability

Demonstrate critical thinking

Proficient with ANSYS FEA and FLUENT software.-Experience with ANSYS command / APDL language.-Experience with plates and shells, FEA experience u

The position involves developing, implementing, and maintaining functionality related toANSYS CFX User Experience capabilities including Pre and Post Processing of data for ANSYSCFX and Fluent programs. Areas of work for this position may include: improvements toexisting capabilities, implementation of advanced features and development of fast algorithms

for post processing products.

In addition, the incumbent will maintain and expand their level of technical excellence in thearea of pre and post processing, user interface technologies, code development and high

performance data structures and algorithms.

The incumbent will contribute to all aspects of software development including design,implementation, validation, and documentation and testing. This position requires the ability towork in a geographically distributed development environment and requires excellentcommunication skills.

Essential Job Functions/Accountabilities: Design, development, optimization and maintenance of features in the products,according to project requirements and established quality standards

Active participation in design brainstorm sessions and team meetings

Tests component functionality based on design specifications

Conducts the unit testing and integration testing for functionality and limits

Researches problems discovered by product testing, product support, and developsolutions to the problems.

Develops and maintains of a high level of technical excellence in the area of pre and post processing and user interfaces.

Ability to work with multiple product teams and across technologies.

Prepares technical documentation of product sub-systems

Provides high-level support to the product support and development staffs.


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Personal Skills:Strong interpersonal and communication skillsAutonomousAble to meet deadlines with good qualityAbel to work in multi-cultural environmentProven Team player able to support project teamsMasters in Mechanical /Aerospace engineering with 4 to 6 years of relevantexperienceStrong engineering fundamentals with good experience in CFD analysisCFD analysis skills using software such as CFX/FLUENT/Star CCM+ and meshgeneration skills using either ICEM/Stat CCM+Expert in 1D hand calculations for CFD AnalysisExposure to programming skills in C/FORTANFamiliarity with propulsion System analysis a plus , but not essentialGood communication & presentation SkillsResponsible for the CFD analysis using software such as CFX/ Fluent/Star CCM+ andmesh generationskills using either ICEM/Star CCM.

Additional Information:Strong Engineering fundamentals with 4 to 6 year of experience in CFD analysisusing software suchas CFX/ Fluent/Star CCM+ and mesh generation skills using either ICEM/Star CCM+,experience on 1dHand calculation for CFD analysis programming skills in C/ Fortan are desired.

Strong engineering fundamentals with 4 to 6 of experience in CFD analysis usingsoftware such asCFX / Fluent / Star CCM+.

Experience on 1D hand calculations for CFD analysis.

Programming skills in C / FORTAN are desired.

Require Bachelor / Masters in Mechanical / Aerospace Engineering.

skills required.doc

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