Model structure effect on static aeroelastic deformation of the NASA CRM
H Bdeiwi, A Ciarella, A Peace, M Hahn - International Journal of …, 2020 - emerald.com
Purpose This paper aims to present a computational aeroelastic capability based on a fluid–
structure interaction (FSI) methodology and validate it using the NASA Common Research …
structure interaction (FSI) methodology and validate it using the NASA Common Research …
Development of reduced order model for dynamic analysis of aircraft via global optimization
O Köse - 2023 - open.metu.edu.tr
Reduced models are often used in the early phases of aircraft design to shorten analysis
times and contribute to the optimization process. In the final stages of aircraft design …
times and contribute to the optimization process. In the final stages of aircraft design …
High-Fidelity Static Aeroelastic Simulations of the Common Research Model
J Navrátil - Flexible Engineering Toward Green Aircraft: CAE Tools …, 2020 - Springer
Current aircraft design leads to increased flexibility of the airframe as a result of modern
materials application or aerodynamically efficient slender wings. The airframe flexibility …
materials application or aerodynamically efficient slender wings. The airframe flexibility …