Aeroelastic Optimization Study Based on the X-56A Model (AIAA 2014-2052)
Creating a Test Validated Structural Dynamic Finite Element Model of the X-56A Aircraft
Flutter Analysis of Aerostructures Test Wing with Test Validated Structural Dynamic Model
Application of Approximate Unsteady Aerodynamics for Flutter Analysis
BASIS FUNCTION APPROXIMATION OF TRANSONIC AERODYNAMIC INFLUENCE COEFFICIENT MATRIX
REDUCED UNCERTAINTIES IN THE ROBUST FLUTTER ANALYSIS OF THE AEROSTRUCTURES TEST WING
Updating the Finite Element Model of the Aerostructures Test Wing Using Ground Vibration Test Data
Build-up Approach to Updating the Mock Quiet Spike™ Beam Model AIAA Paper 2007-1776 CD-ROM Number 7
Quiet Spike™ Build-Up Ground Vibration Testing Approach AIAA Paper 2007-1775 CD-ROM Number 8