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

Posted at - Sep 19, 2021

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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 15, 2017 Cedric Bachmann
from Geneve, Switzerland

Skills & Expertise Required

ANSYS Finite Element Analysis Mechanical Engineering 

Candidate shortlisted and hiredHiring open till - Sep 26, 2021

Work from Anywhere
40 hrs / week
Fixed Type
Remote Job
$27.84
Cost

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