NASA aiaa 99 1262

AIAA REDUCED ORDER MODELS BASED ON LINEAR AND NONLINEAR AERODYNAMIC IMPULSE RESPONSES Walter A. Silva Aeroelasticity B...

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AIAA

REDUCED ORDER MODELS BASED ON LINEAR AND NONLINEAR AERODYNAMIC IMPULSE RESPONSES

Walter A. Silva Aeroelasticity Branch NASA Langley Research Center Hampton

Presented at the AIAA/ASE/ASCE/AHS/ASC 40th Structures, Structural Dynamics, and Materials Conference April 12-15, 1999 St. Louis, Missouri

AIAA Paper No. 99-1262