aircraft structural analysis
Budget: $25 – $50 USD
I am looking for an expert to provide aircraft structural analysis on a private single engine experimental aircraft with the focus on proof of structure to FAA CAR 3 or part 23 requirements for cradle type engine mount and attachment points on air frame, as well as analysis required to meet same basis for increase in max weight limit for small baggage area.
Should current structure not meet requirements, will additionally require input on modifications needed.
Process can be FEA with detailed report demonstrating compliance per above basis.
The primary goal of this analysis is to compare my experimental aircraft structural strength to FAA requirements for a standard certified aircraft of same category.
This project requires knowledge about aircraft and structural design and analysis, as well as experience with aircraft structural analysis. Successful completion of the project requires the ability to produce a detailed report with accurate results. This project is suitable for a freelancer who have the necessary skills and knowledge and are committed to providing a detailed analysis and report.
Should current structure not meet requirements, will additionally require input on modifications needed.
Process can be FEA with detailed report demonstrating compliance per above basis.
The primary goal of this analysis is to compare my experimental aircraft structural strength to FAA requirements for a standard certified aircraft of same category.
This project requires knowledge about aircraft and structural design and analysis, as well as experience with aircraft structural analysis. Successful completion of the project requires the ability to produce a detailed report with accurate results. This project is suitable for a freelancer who have the necessary skills and knowledge and are committed to providing a detailed analysis and report.