Organizational Unit:
Aerospace Systems Design Laboratory (ASDL)
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An architecture model of the U.S. air transportation network
Resilience-enhanced control reconfiguration for autonomous systems
A framework for concurrent design and route planning optimization of unmanned aerial vehicle based urban delivery systems
A numerical investigation into the aerodynamic effects of tubercles in wind turbine blades
A reduced-order modeling methodology for the multidisciplinary design and analysis of boundary layer ingestion configurations
A methodology for the prediction of non-volatile particulate matter from aircraft gas turbine engine
A bi-Level framework for aircraft design uncertainty quantification and management
An architecture-based growth approach for industrial gas turbine product development
An unsteady aerodynamics reduced-order modeling method for maneuvering, flexible flight vehicles
Fidelity assessment for model selection (FAMS): A framework for Initial comparison of multifidelity modeling options