11 Hand Calculations Jobs

The ideal candidate should possess a good understanding of engineering basics and a thorough knowledge of the product life cycle and downstream activities. Strong expertise in Ansys, Nastran, Patran procedures, and methods is essential, along with experience in wings, fuselage, and high lift structures. Proficiency in drawing reading and G&DT is required. The candidate must hold a Bachelor of Engineering degree in Mechanical Engineering and have a basic knowledge of fatigue, finite element analysis, and manufacturing processes. Good knowledge of aero engine components, stack-up layout and calculations, manufacturing processes including heat treatment and welding, as well as hand calculations, is necessary. Familiarity with GD&T, assembly techniques, and assembly processes is essential. Preferred qualifications include experience in ISAMI Ansys, Nastran, Patran, and aero structure component analysis.,

As an FEA Engineer in Heavy Engineering, you should have 4 to 8 years of experience and hold a BE/B.Tech or ME/M.Tech degree. Your expertise should lie in ANSYS Workbench, Ansys Classic, Nonlinear Analysis, Static Analysis, Dynamic Analysis, Composite Analysis, Rotor Analysis, Spaceclaim, Hand Calculations, Weld calculations, DesignModeler, and Finite Element Analysis. Your primary focus will be on industries such as Industrial, Heavy Industries, Construction Equipment, Oil & Gas, and Energy/Power sector, excluding Aerospace and Automotive domains. Your responsibilities will revolve around Simulation and Analysis, including structural, thermal, dynamic, and fatigue analysis using FEA tools. You will be required to develop and validate finite element models, conduct linear and nonlinear analysis, and perform crash, impact, and durability simulations based on industry needs. Additionally, you will be responsible for Model Preparation and Meshing by creating high-quality finite element meshes, simplifying complex geometries, and applying appropriate boundary conditions, loads, and constraints. Design Optimization will be a key aspect where you collaborate with design and product development teams to suggest material changes, thickness adjustments, and structural modifications for performance enhancement and cost reduction. Your role also entails Documentation and Reporting, where you will prepare detailed technical reports, present findings to stakeholders, and maintain FEA documentation for future reference and regulatory compliance. To excel in this position, you must be proficient in ANSYS Workbench and ANSYS Classic, possess strong communication skills, work independently, and adhere to quality standards. Having a background in ASME, API, EN, and BS standards is essential, and knowledge of HyperMesh and Abaqus is a plus. Your ability to parameterize models, develop macros, and effectively communicate design recommendations will be crucial in this Digital Product Engineering (H&I) role.,

As an ideal candidate for this role, you will be proficient in NX CAD software, possess a strong understanding of Geometric Dimensioning and Tolerancing (GD&T), and be experienced in Stackup Analysis. Your knowledge of Aero engine fundamentals will be a valuable asset in this position. You will be responsible for creating and modifying Engineering Drawings, as well as handling Nonconformances Disposition effectively. Additionally, you should have expertise in both 2D and 3D Modelling, along with the ability to perform Hand Calculations. A fundamental understanding of Strength of Materials is also required for this role. Your attention to detail and precision will be crucial in ensuring the accurate and efficient completion of tasks related to these skills.,

Position Overview: We are seeking a Senior Aero structure Stress Analyst to join our dynamic engineering team. The ideal candidate will be responsible for conducting stress and structural analyses on aerospace components and systems to ensure they meet safety, performance, and regulatory standards. This position requires a deep understanding of structural mechanics, aerodynamics, materials science, and the ability to collaborate with cross-functional teams to solve complex engineering challenges. Key Responsibilities: Perform detailed static, dynamic, fatigue, Damage tolerance and failure analysis on aero structures, including wings, fuselage, landing gear, Floor beam, Doors and other aircraft components. Utilize Finite Element Analysis (FEA) software, such as HYPERMESH, NASTRAN, PATRAN ABAQUS, or ANSYS, to model and analyse structural performance under various loading conditions. Ensure compliance with aerospace industry standards, including FAA, EASA, and military regulations, and participate in design reviews. Experience on Airbus and Boeing Aircraft structures is an added advantage. Develop and validate analytical methods using excel and Macros techniques to predict the behaviour of structural components. Work closely with design engineers to provide input on material selection, design changes, and manufacturing processes to optimize structural performance and minimize weight while maintaining safety. Support testing and validation efforts, including static and fatigue testing, to validate theoretical analyses. Lead technical reports and documentation to communicate analysis results, design recommendations, and compliance to regulatory bodies and customers. Preparing the certification standard report with detailed explanations of procedures followed for analyzing a structure to support PDR and CDR. Include all the mitigations and summarize Reserve factor in the report Mentor and provide guidance to junior engineers and analysts. Collaborate with cross-functional teams (materials, design, systems, etc.) to ensure integrated, efficient, and safe structural designs. Identify and address structural performance risks, and provide solutions to improve the overall reliability and performance of aero structures. Participate in customer-facing discussions and presentations related to structural design and analysis. Conduct optimization studies to enhance structural efficiency, reduce weight, and improve manufacturability of fuselage components. Explore design alternatives to achieve optimal performance Qualifications: Bachelor's, Master's,in Aerospace Engineering, Mechanical Engineering, or a related field. 10+ years of experience in stress analysis and design of aero structures, preferably in the aerospace industry. In-depth knowledge of structural analysis methods, including finite element modelling (FEM), classical hand calculations, and failure theories. Proficient in FEA tools such as NASTRAN, ABAQUS, ANSYS, or similar software. Strong understanding of aerospace materials, including composites, metals, and advanced alloys. Experience in the analysis of static, dynamic, fatigue, and fracture mechanics. Familiarity with aircraft systems and the integration of structures with other aircraft systems. Solid understanding of aerospace regulatory standards and certifications (e.g., FAA, EASA). Skills Required Stress Calculations, Hand Calculations, Structural Analysis, Finite Element Analysis (FEA) Location Hyderabad, India Desirable Skills Stress Calculations, Hand Calculations, Structural Analysis, Finite Element Analysis (FEA) Designation Associate

As a skilled professional, you will be responsible for utilizing NX CAD software to create and modify engineering drawings. Your expertise in Geometric Dimensioning and Tolerancing (GD&T) will be essential in ensuring the accuracy and quality of the designs. Additionally, you will conduct stackup analysis to evaluate the dimensional variations within assemblies. A solid understanding of aero engine fundamentals is required to effectively contribute to the design process. Your proficiency in 2D and 3D modeling will be crucial in visualizing and developing innovative solutions. You will also be tasked with performing hand calculations and applying basic knowledge of strength of materials to validate the designs. Handling nonconformances and providing timely disposition will be part of your daily activities. Your attention to detail and problem-solving skills will be instrumental in identifying and resolving any discrepancies in the design process. By collaborating with cross-functional teams, you will ensure that the final products meet the required specifications and standards.,

You will be part of a dynamic team as a Mechanical Design Engineer - Aero Engine for our esteemed client in Bangalore. With 5-15 years of experience, you will play a crucial role in the design and development of components and assemblies for gas turbine aeroengines. Your expertise in stack-up analysis, hand calculations, stress analysis, Bruhn method, Dolly design, and gas turbine will be essential for this role. Your responsibilities will include supporting the design and development process for gas turbine aeroengines of various sizes, performing stack-up analysis, finalizing component designs for RFQ and raw material release, selecting specifications for components, establishing Freebody diagrams, conducting buckling calculations using the Bruhn method, analyzing bolt joints, and performing stress analysis for components. Additionally, you will be designing Dolly fixtures for assembly and test processes, ensuring precise and efficient engineering solutions in a challenging work environment. You should possess strong skills in stack-up analysis, envelope finalization, specification selection, Freebody diagram establishment, buckling calculation, bolt joint analysis, geometry check, stress analysis, hand calculations, and material selection. Desired skills include experience in aero or marine engine component design, requirement analysis, concept generation, DFMEA, mechanical hand calculations, life cycle calculations, engineering productivity, service productivity improvement, product performance management, static and dynamic analysis, and GD&T. The ideal candidate will have 5-15 years of experience in design and development of gas turbine aeroengines, with a background in aeroengine design and excellent skills in performing hand calculations for stress, especially in gas turbine applications. This is a full-time position with a Day shift schedule from Monday to Friday, and the work location is in person. The benefits include Provident Fund.,

Perform high-quality mesh generation for structural analysis using Hypermesh and Patran . Develop and refine GFEM and DFEM models for various components and assemblies, ensuring mesh quality and compliance with CAE standards. Prepare models for static, dynamic, and thermal FEA simulations. Interpret and apply engineering drawings and CAD data to build accurate finite element models. Ensure mesh quality and convergence to meet analysis requirements. Ensure adherence to customer-specific FEM guidelines and industry best practices. Collaborate closely with design, simulation, and test teams to validate and iterate FE models. Document meshing processes, model assumptions, and preprocessing methodologies. Troubleshoot and resolve issues related to meshing and model setup. Familiarity with optimization techniques for FE modeling. Required Skills & Qualifications: Bachelor's or Master's degree in Mechanical, Aerospace, or related engineering field. 3 to 7 years of relevant CAE experience , with a focus on meshing and preprocessing. Strong command of Hypermesh and Patran for shell and solid meshing. Hands-on experience in GFEM and DFEM meshing techniques and standards. Solid understanding of FEA fundamentals, material properties, and boundary conditions. Familiarity with CAD software (e.g., CATIA, NX) for model extraction and cleanup. Excellent problem-solving and communication skills. Ability to manage multiple tasks and meet tight deadlines. Proactive attitude towards continuous improvement and learning. Preferred: Exposure to solver environments like OPTISTRUCT , NASTRAN , ABAQUS for FE model set-up Experience with scripting or automation (e.g., TCL, Python) in preprocessing. Knowledge of aerospace or automotive domain-specific CAE workflows.

Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Required Skills & Qualifications: Bachelor's or Master's degree in Mechanical, Aerospace, or Structural Engineering. 3 to 7 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Solid understanding of fracture mechanics , crack growth behaviour , and fatigue life prediction methodologies. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team. Attention to detail and accuracy in calculations and reporting. Proactive attitude towards continuous improvement and learning.

Roles and Responsibilities: Work with offshore and global teams to understand project scope including analysis domain, boundary condition, material models, type of analysis etc. Active Coordinator for multiple groups that include Design, Aerodynamics and Structures teams for Project specific inputs Ability to work autonomously and prioritize multiple projects Review technical presentations, interpret the results and present the same to Customer Expertise in dealing with Design and Technical Discipline reviews Responsible for ensuring 100% quality and on-time delivery Conduct project review meetings to share the lessons learned and best practices to the team to improve the quality Responsible for providing alternative solutions on field issues Responsible forprocess improvements by developing Automation tools Work on complex CAE problems to assist product development Prepare Technical proposals and Business cases for new process improvement areas Perform Design Modifications as per need and validating the same with FEA Demonstrate Excellent Technical, Project Management, Interpersonal and Problem solving skills Mandatory skills: Minimum 6 years of experience in Stress analysis of Aero engine components (Rotors, Cases, Stators and Externals) using commercial Finite Element Analysis tool. Expertise in handling various structural analysis tools preferably ANSYS Classic, Ansys Workbench, Hypermesh etc 2D & 3D Finite Element modeling of simple, moderate and complex components (Hexahedral & tetrahedral elements) using ANSYS-APDL or Workbench Linear and non-linear static stress analysis (Geometric, Material and contact Linearity) using ANSYS-APDL or Workbench Modal, Harmonic and transient Dynamic stress analysis using ANSYS-APDL or Workbench Strength, stability and Durability of components Damage tolerance analysis to estimate fracture life Should able to develop/modify APDL Macros Should able to build/update FE Models in HyperMesh. Desired Skills: Experience in scripting using Matlab, VB,TCL/Tk, Python is an added advantage Knowledge of Hand Calculations, Standards and Design codes is an added advantage Basic Knowledge of CAD tools is and added advantage

Bachelor's or Master's degree in Mechanical, Aerospace, or related engineering field. 7 to 15 years of relevant CAE experience , with a focus on meshing and preprocessing. Strong command of Hypermesh and Nastran/ Patran for shell and solid meshing. Hands-on experience in GFEM and DFEM meshing techniques and standards. Perform Strcutural Analysis Hand calculation for static stress checks like Buckling, crippling, Lug analysis, fastener check using classical methods Solid understanding of FEA fundamentals, material properties, and boundary conditions. Familiarity with CAD software (e.g., CATIA, NX) for model extraction and cleanup. Excellent problem-solving and communication skills. Ability to manage multiple tasks and meet tight deadlines.

Currently, we are looking for highly competent and dedicated Engineer / Senior Engineer - Mechanical Design - Inventor . to join our efficient and friendly team. As part of ENABL India, you will become a member of a team of exceedingly motivated and skilled engineers, working for some of the major companies Globally, within the wind industry. Immediate Joiner's Preferred Qualifications: Bachelor / Master's degree in Mechanical Engineering Minimum 7 - 10 yrs experience in Product design using Autodesk Inventor in Cranes / Lifting Tools / Heavy Engineering Industry Experience in Mechanical design and specification in compliance with relevant international standards Experience in a multi-cultural environment Competencies: In-depth knowledge in Structural Mechanics is essential Experience in 3D-Modeling and 2D-drafting, e.g. using Autodesk Inventor PDMLink and project execution through SAP/ERP/ECM systems Expereince in Skeleton Modeling Work experience in GD&T Work Experience/or Exposure to lifting tools and structures in an assembly Factory Knowledge on FEA (E.g. ANSYS/Pro-Mechanica) is a plus Knowledge of Wind turbines / Heavy lifting/ Transportation equipment Exposure or Experience with International engineering standards like ASME/EN/ISO etc.(Eurocode) Exposure to CE marking/DFMEA/risk assessment etc. needed for product development Regards Talent Acquisition Team