THE AIRCRAFT NOISE SIMULATION WORKING GROUP (ANSWR) — V2 AIRCRAFT RESULTS
A DISCRETE ADJOINT FRAMEWORK FOR LOW-BOOM SUPERSONIC AIRCRAFT SHAPE OPTIMIZATION (AIAA 2017-3326)
AERO-STRUCTURAL OPTIMIZATION OF THE NASA COMMON RESEARCH MODEL (AIAA 2017-4145)
Pairwise Trajectory Management (PTM): Concept Overview (AIAA 2017-3933)
Loads Analysis and Structural Optimization - A Parameterized and Integrated Process