Remote Architecture Job In Engineering And Architecture

Topological Optimization project

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Its a Vans 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 recuiter
Member since Mar 14, 2020
Shivani Aggarwa
from Gegharkunik, Armenia

Skills & Expertise Required

ANSYS Finite Element Analysis Mechanical Engineering 

Open for hiringApply before - Nov 8, 2024

Work from Anywhere

40 hrs / week

Fixed Type

Remote Job

$38.09

Cost

Offer to work on this project closes in 58 days!
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