High-Fidelity Computational Simulation of Nonlinear Fluid-Structure Interaction Problems
Abstract
Key issues: 1) High-fidelity computational aeroelastic methods are needed to address UAV fluid/structure interaction issues; 2) These schemes will need to be very efficient to address long temporal integration requirements; 3) Well documented, basic experiments are still needed for code validation; 4) Additional disciplines may need to be added to adequately address the fluid/structure interaction issues.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 05, 2002
- Accession Number
- ADA428840
Entities
People
- Raymond E. Gordnier
Organizations
- Air Force Research Laboratory