Rapid Prediction of Worst-Case Gust Loads Following Structural Modification
- 1 February 2014
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 52 (2), 242-254
- https://doi.org/10.2514/1.j052031
Abstract
An approach to reduce the computational effort required to determine the worst-case gust loads for aircraft is described, specifically when structural modifications are included as part of the design process. The Sherman–Morrison–Woodbury formula is employed to determine the gust response of the modified structure using a reanalysis approach and to undertake an efficient modal reanalysis. The approach is demonstrated successfully using a simple wing and full-scale aircraft finite-element models to determine the worst-case “1−cosine” gust following structural modification. Savings of about 56% were achieved for gust-response computations and 50% for the modal reanalysis.This publication has 24 references indexed in Scilit:
- Reanalysis and sensitivity reanalysis by combined approximationsStructural and Multidisciplinary Optimization, 2009
- Introduction to Aircraft Aeroelasticity and LoadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2007
- Efficient Dynamic Reanalysis of StructuresJournal of Structural Engineering, 2007
- Approximate Vibration Reanalysis of StructuresAIAA Journal, 2003
- A new method of structural modal reanalysis for topological modificationsFinite Elements in Analysis and Design, 2002
- Fast exact linear and non‐linear structural reanalysis and the Sherman–Morrison–Woodbury formulasInternational Journal for Numerical Methods in Engineering, 2001
- Structural Modal Reanalysis of Topological ModificationsShock and Vibration, 1999
- Structural Loads Analysis for Commercial Transport AircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Structural modification with frequency response constraints for undamped mdof systemsComputers & Structures, 1990
- Gust Loads on Aircraft: Concepts and ApplicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988