Technique employing the modified SIMP topology optimization method to determine the panel-to-panel support bracket position in a spacecraft body
Published: 24.01.2024
Authors: Borovikov A.A., Tushev O.N.
Published in issue: #1(145)/2024
DOI: 10.18698/2308-6033-2024-1-2331
Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft