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About A Cfd/Doublet Lattice/Md Nastran Calculation of Static Aeroelastic Trim and Structural Loads
This document describes a new hybrid process for static aeroelastic analysis that combines computational fluid dynamics (CFD) with doublet lattice methods. The process utilizes nonlinear aerodynamic data from CFD or wind tunnel tests with aeroelastic corrections from doublet lattice or other panel methods. The process performs a nonlinear trim calculation efficiently while incorporating aerodynamic nonlinearities, flexible corrections, and general trim specifications. Statistics on problem size and CPU times indicate the process can be applied to real-world design tasks affordably.
Detailed Information
| Author: | ['Hrishikesh Phadke'] |
|---|---|
| Publication Year: | 2022 |
| Pages: | 12 |
| Language: | English |
| Format: | |
| Price: | FREE |
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