Different types of structural and aerodynamic nonlinearities commonly encountered in
aeronautical engineering are discussed. The equations of motion of a two-dimensional …

Domain decomposition approaches require efficient interface techniques when fluids and
structures are solved in independent computational domains for aerospace applications …

New capabilities have been developed for a Navier-Stokes solver to perform steady-state
simulations more efficiently. The flow solver for solving the Navier-Stokes equations is based …

The loose coupling of computational Ŋ uid dynamics and computational structural dynamics
solvers introduces some problems related to the information transfer between the codes …

A methodology for the coupling of an advanced computational fluid dynamics method based
on an overset grid flow-solver and an advanced computational structural dynamics method …

With advanced subsonic transports and military aircraft operating in the transonic regime, it
is becoming important to determine the effects of the coupling between aerodynamic loads …

The high level of maturity reached in many computational disciplines, prompts for the study
of new multidisciplinary applications, of great importance for engineering purposes. Such is …

4th Symposium on Multidisciplinary Analysis and Optimization : Coupled finite-difference/finite-element
approach for wing-body a Page 1 AIAA-92-4680-CP COUPLED FINITE-DIFFERENCE/FINITE-ELEMENT …

The requirement to deal with arbitrarily complex fluid and structural models, geometries and
discretization techniques, introduces a number of problems associated to the transfer of …

The objective of this work is to demonstrate a computationally efficient, high-fidelity,
integrated static aeroelastic analysis procedure. The aerodynamic analysis consists of …