Vehicle dynamic control of a passenger car applying flexible body model
Virtual operational strength analysis for commercial vehicles
Development of Advanced Computational Aeroelasticity Tools at NASA Langley Research Center
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Dynamic Analysis of a Flexible Spacecraft with Rotating Components. Volume 3: Program Code
Techniques Used in Aeroelasticity for the Presentation of Aircraft Flight
Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters
Response of Flexible Space Vehicles to Docking Impact. Volume 2 - Numerical Investigation
Near Resonant Vibration Tests of an Orbiting Flexible Spacecraft: Theory, Design and Simulation
Study of APOLLO Water Impact. Volume 6 - User'S Manual - Interaction Final Report