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