Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow
Stability and Control CFD Investigations of a Generic 53 Degree Swept UCAV Configuration
Development and Testing of Control Laws for the Active Aeroelastic Wing Program
Optimization Methods Applied to the Aerodynamic Design of Helicopter Rotor Blades
Small-Scale Tiltrotor Model Operating in Descending Flight
Determination of Stores Pointing Error Due to Wing Flexibility under Flight Load