All Stories

  1. Classical Flutter Analysis of X-57 Aircraft Mod II, III, and IV Configurations
  2. Finite Element Model Tuning Using Analytical Sensitivity Values
  3. Linear and Geometrically Nonlinear Structural Shape Sensing from Strain Data
  4. Shape Sensing for Wings with Spars and Ribs using Strain Data
  5. Jig-Shape Optimization of Low-Boom Supersonic Aircraft
  6. Jig-Shape Optimization of a Low-Boom Supersonic Aircraft
  7. Unsteady Aerodynamic Force Sensing from Strain Data
  8. New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
  9. Wing Shape Sensing from Measured Strain
  10. Acceleration and Velocity Sensing from Measured Strain
  11. Creating a Test-Validated Finite-Element Model of the X-56A Aircraft Structure
  12. Mass Balancing Optimization Study to Reduce Flutter Speeds of the X-56A Aircraft
  13. Delta Adaptive Flexible Motion Control for the X-56A Aircraft
  14. Aeroelastic Tailoring Study of an N+2 Low-boom Supersonic Commercial Transport Aircraft
  15. Wing Shape Sensing from Measured Strain
  16. Aeroelastic Optimization Study Based on the X-56A Model
  17. Creating a Test Validated Structural Dynamic Finite Element Model of the X 56A Aircraft