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