THE AIRCRAFT NOISE SIMULATION WORKING GROUP (ANSWR) - TOOL BENCHMARK AND REFERENCE AIRCRAFT RESULTS
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)
REDUCTION OF AIRFRAME NOISE COMPONENTS USING A DISCRETE ADJOINT APPROACH (AIAA 2017-3658)
An Emission-Minimizing Vehicle Routing Problem with Heterogeneous Vehicles and Pathway Selection
The Value of Semi-Empirical Analysis Models in Aircraft Design (AIAA 2015-2486)
A Discrete Adjoint Framework for Unsteady Aerodynamic and Aeroacoustic Optimization (AIAA 2015-3355)
Evolutionary Genetic Diversification, Demography, and Conservation of Bartram's Bass
Discrete Adjoint Approach for Aeroelastic Design Optimization
Quantifying Uncertainty Across Fidelity Levels in the Design of Aerospace Systems
Estimation of Stability and Control Derivatives for a Piper Cub J-3 Remotely Piloted Vehicle