I will provide you a simple aircraft wing model (.stp file).
I want to complete a masters level thesis titled "Structural Optimization of Light Wight Aircraft Wing"
1. Analyse the wing for take-off of Stress conditions ( initial loading conditions)
2. Perform Topology and Weight Optimization of Wing
3. Write a Masters of Engineering Level Thesis for this project
Please bid if you can do this job sincerely. Upon award this project to you, I will create payment (milestones) to you but I will pay (release the milestone) only after getting all things done by you.
Please bid you all agreewith all above and say Design123 at start of your bid so that I could understand that you read all of this carefully.
Design123 Project Methodology:- Thanks for viewing my proposal, please have a look into the profile. Objective :- Topology and weight Optimization of Aircraft Wing Expected Inputs:- parameter details. Plus
11 freelance font une offre moyenne de ₹12198 pour ce travail
Greetings! Thank you for the opportunity to work on this project. I hold a Bachelor of Business Administration and a Master of Business Administration degree and will provide you with original, compelling content Plus
Professional aerospace and controls domain engineer here ....................................................................................
Design123 Hello, sir. I am a TECHNICAL WRITER with 2 years’ experience of working on projects including dissertation, thesis, research proposals, research papers, assignments, project management and business plans. I Plus
MY PROPOSAL Title: 3D Modelling. Short Description: I am 3D generalist specialized in developing high quality photo-realistic 3D render images, 2D & 3D animations, organic and non-organic rigging, graphic desi Plus
Design123 Hi, I found your project and I see what my skills are suitable for you. I'm a physicist, now I'm studying for my PhD, I have worked for official representative of CD-Adapco in Russia for two years, I have do Plus
We can do the project which you have described ,We are stress /CAE engineers Our expertise includes , Meshing/modeling/Linear/Non-linear /Crash/Dynamic Analysis /Design Optimization And Topology as well . Please Plus
i have done the exact task with airbus in the past in my career. I will give the break up how we can work around. Tools - hypermesh/nastran/Patran/excel/ inputs - limit loads and cad. the work will be comple Plus
I have worked on hyperworks related with topology optimization . Also this can be performed in ansys workbench. Hence kindly send the load details with the model for further negations.