G. Brown

发表

Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter

Gregory W. Brown, C. Farhat, P. Geuzaine, 2003 .

Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions

Charbel Farhat, Chuck Harris, Philippe Geuzaine, 2003 .

Mesh partitioning for implicit computations via iterative domain decomposition: Impact and optimization of the subdomain aspect ratio

Gregory W. Brown, C. Farhat, N. Maman, 1995 .

Nonlinear Flutter Analysis of an F-16 in Stabilized, Accelerated, and Increased Angle of Attack Flight Conditions

Charbel Farhat, Chuck Harris, Philippe Geuzaine, 2002 .

Three-field-based nonlinear aeroelastic simulation technology - Status and application to the flutter analysis of an F-16 configuration

Charbel Farhat, Philippe Geuzaine, Gregory W. Brown, 2002 .

Extending Sensitivity-Based Updating to Lightly Damped Structures

François M. Hemez, Charbel Farhat, Gregory W. Brown, 1997 .

EVALUATING THE EFFECT OF LIMITED INSTRUMENTATION ON THE UPDATING OF FINITE ELEMENT MODELS

Charbel Farhat, Gregory W. Brown, Frangois M. Hemez, 1998 .

OVERCOMING DIFFICULTIES IN THE UPDATING OF FE MODELS FOR INDUSTRIAL APPLICATIONS

J. Duysens, G. Brown, Charbel FarhatJ, 1997 .