UAS Fuselage Structural Parameterisation

@Ekarthaan

Hi ahmedh0245, This is quite similar to a project I delivered last week, so I can jump straight into execution. Ready to start immediately. 1) Preferred solver path: ANSYS Workbench + ACP, SimScale, or SolidWorks Simulation—and should impact be modeled explicitly (transient) or via a calibrated quasi‑static energy surrogate? 2) Please provide load inputs: wing/tail reaction magnitudes and locations, landing/ground impact energy or velocity, payload/battery mass and CG, and target FoS/allowables (strain/strength) plus fatigue duty cycle. Use a master skeleton: one Control Sketch + Design Table drives loft, cross‑section, skin‑thickness law, rib pitch, bulkhead count/offsets, and insert patterns; all children reference skeleton datums to survive ±10% length edits. In FEA, adopt shell+laminate modeling (ACP): orthotropic cards with ply rules as parameters, named selections tied to CAD persistent IDs, and a study template (rib spacing/bulkhead placement/ply thickness) for rapid what‑ifs. Action Plan: 1) Requirements: confirm geometry envelopes, loads, impact/fatigue definitions, manufacturing route, laminate candidates. 2) CAD: build skeleton + Design Table; create fuselage surfaces/solids, ribs/bulkheads/inserts from driven planes; verify regen at ±10% Best Regards, Sid

@miskinarati

Hi there, I would be happy to assist with the UAS fuselage structural parameterisation project. With strong experience in ANSYS, parametric modeling, and aerospace structural analysis, I can develop a robust and scalable solution for your requirements. Approach: Create parametric CAD/FEA model of fuselage (frames, longerons, skin) Define key design variables (thickness, materials, geometry, stiffener spacing) Setup ANSYS Workbench parametric study using DesignXplorer/APDL Apply realistic load cases (aerodynamic loads, payload, mounting conditions) Perform static, modal, and sensitivity analysis Automate parameter variation and response evaluation Deliverables: Fully parameterized ANSYS model Input-output relationship for key structural parameters Stress, deformation, and modal results for design variants Optimization-ready setup with clear documentation Timeline: To be determined after discussing project scope. Budget: Open to negotiation based on complexity. Looking forward to collaborating on this project. Let’s connect to discuss further. Best regards, Arati M.

@sahildogra222

Hello there , I’ve carefully checked your requirements and really interested in this job. I’m working as a freelance graphic designer with U.S. and European teams. I’m offering best quality and highest performance at lowest price. I can complete your project on time and your will experience great satisfaction with me. I have rich experienced in Structural Engineering, Design Optimization, Finite Element Analysis, Solidworks, Mechanical Engineering, 3D Design, Ansys and 3D Modelling. For more information about me, please refer to my portfolios. I’m ready to discuss your project and start immediately. Looking forward to hearing you back and discussing all details.. Please respond at your earliest convenience

@frosthp

Hello, I can create for you SW model for ansys, I am use ANSYS, I will prepare it for good mesh, without interference, small gaps, sharp edges, this model will easy mesh, set up contacts etc. Please feel free to contact me.

@Is88

I am an experienced engineer specializing in ANSYS simulations, offering advanced computational modeling and analysis services to support design validation, optimization, and failure prevention. Using ANSYS Workbench, Mechanical, and Fluent, I can deliver accurate results through structural, thermal, and fluid flow studies, vibration analysis, and failure prediction. Specialized in; 1) 3D model setup and meshing in ANSYS 2) Static structural and thermal analysis 3) CFD simulation for fluid flow and heat transfer 4) Modal and harmonic vibration analysis 5) Fatigue and failure evaluation 6) Optimization and design improvement recommendations 7) Comprehensive technical report with results and conclusions

@muhannadbukhamse

Hi there, I can develop a robust, fully parametric fuselage model tailored for rapid iteration and structural validation, aligned with your UAS Challenge goals. Scope of Work: ✅ Parametric SolidWorks fuselage with control sketch/design table ✅ Carbon fibre laminate material definition (adjustable ply/thickness) ✅ Clean CAD-to-FEA workflow (ANSYS/SimScale/native) ✅ Load cases for impact, load-bearing, and fatigue ✅ Mesh-ready model with stable rebuild (±10% length) ✅ Validation report with assumptions and safety factors I can perform the project end-to-end with reliable and editable results. Best Regards,

@StarSpark3D

As a highly skilled 3D modeling engineer specialized in the robust design of mechanical parts, I am confident in my ability to not only meet, but exceed your expectations for this project. I have extensive experience working with SolidWorks, the very software you mentioned that you'd prefer your workflow start in, propelling your vision from ideation to validation seamlessly. My vast knowledge in materials selection and specific skill with carbon-fiber laminates will empower me to deliver a fully-parameterized fuselage model that can withstand various flight-related stressors. Moreover, the driving dimensions of the fuselage model will be clearly labeled and manipulable from a single control sketch or design table—a defining factor for a thorough analysis of varying configurations.

@hayat38402

Hi, how are you doing? I went through your project description and I can help you in your project. your project requirements perfectly match my expertise. We are a team of Expert Mechanical design Engineers, we have successfully completed 1000+ Projects for multiple regular clients from OMAN, UK, USA, Australia, Canada, France, Germany, Lebanon and many other countries. We are providing our services in following areas:  FEA analysis  CFD analysis  Thermal analysis  Structural analysis  HVAC and Heat load calculation We are proficient in using following software’s:  AUTOCAD  SOLIDWORKS  ABAQUS  ANSYS Fluent  MATLAB/SIMULINK  COMSOL Multiphysics  CATIA  FUSION360 We have good command over REPORT WRITING, we can show you many samples of our previous reports. We can discuss further details in the message box.

@afshan2176

Hello , I've just reviewed your project description regarding the UAS Fuselage Structural Parameterisation and I'm confident in my ability to meet your expectations. With over 7 years of experience as a Senior Graphic Designer, I possess a strong skill set in Structural Engineering, Design Optimization, Solidworks, Mechanical Engineering, 3D Design, Finite Element Analysis, Ansys and 3D Modelling I kindly request you to take a moment from your busy schedule to explore our portfolio, where you can see the quality of my work and read feedback from previous clients: [Portfolio Links] https://www.freelancer.com/u/afshan2176 Could you please specify the final file formats you'll require? Feel free to award me the project so that we can discuss it further. Looking forward to connecting with you. Best regards, Afshan Z.

@AhmadArmaghan

I can create a clean, fully parametric fuselage model tailored for your IMechE UAS Challenge entry, keeping structural integrity as the core focus. The design will be built in SolidWorks with a single control sketch and design table, allowing you to easily adjust key parameters like length, diameter, and skin thickness without breaking references. I will also include a carbon fibre laminate material setup with editable properties to match evolving ply schedules. The workflow will transition smoothly into FEA (ANSYS/SimScale or native), with predefined load cases covering impact resistance, load capacity, and fatigue. You’ll receive a ready-to-run simulation setup for fast iteration on ribs, bulkheads, and inserts. Deliverables include the parametric CAD model, material library, FEA setup, and a concise validation report. The model will be tested for ±10% geometry changes to ensure stability and reliable results.