A DISCRETE ADJOINT FRAMEWORK FOR LOW-BOOM SUPERSONIC AIRCRAFT SHAPE OPTIMIZATION (AIAA 2017-3326)
REDUCTION OF AIRFRAME NOISE COMPONENTS USING A DISCRETE ADJOINT APPROACH (AIAA 2017-3658)
A Discrete Adjoint Framework for Unsteady Aerodynamic and Aeroacoustic Optimization (AIAA 2015-3355)