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Required ANSYS,Finite Element Analysis,Mechanical Engineering freelancer for Topological Optimization project job

Posted at - Jun 13, 2023

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Its a Van's Aircraft RV-4. The wing has NACA 23015 airfoil shape. Max takeoff weight 1550 lbs. wing loading is 14.09 lbs per sq ft. Max speed of aircraft should not exceed 180 mph. Wingspan 7 m. One wing is 2.8 m. Total Ming area is 10.2 sq m. Use aluminum alloy as material.
As per my calculations pressure on the wing at 18000 ft at -30 degree Celsius would be 45000 Pa.
I want you to send me the result file with the objective and objective constraints you will choose.
Circled one should be the final shape after optimization or something similar.
You show me the results and you will get paid.

About the recuiterMember since Sep 7, 2017 Manas Pradhan
from Maharashtra, India

Skills & Expertise Required

ANSYS Finite Element Analysis Mechanical Engineering 

Open for hiringApply before - Jun 12, 2024

Work from Anywhere
40 hrs / week
Fixed Type
Remote Job
$38.37
Cost

Offer to work on this project closes in 45 days!
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