The Liebherr Fully Integrated FCS Design - A Case Study
2010-9220 Fast Estimation of Top-Level Aircraft Requirement Impact on Conceptual Aircraft Designs
DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK
Economic Assessment of Morphing Leading Edge Systems in Conceptual Aircraft Design
Economics of Laminar Aircraft Considering Off-Design Performance
An Integrated Environment for Preliminary Aircraft Design and Optimization
Influence of Off-Design Performance on the Design of Aircraft with Laminar Flow Technology
Aircraft Cost Model for Preliminary Design Synthesis
Gains in Fuel Efficiency: Multi-Stop Missions vs. Laminar Aircraft
Conceptual Design of a Battery-Powered High Lift System for Single-Aisle Aircraft (AIAA 2014-0378)
ASSESSMENT OF AN INNOVATIVE MORPHING LEADING EDGE CONSIDERING UNCERTAINTIES IN CONCEPTUAL DESIGN
Impact of an Innovative Quiet Regional Aircraft on the Air Transportation System