Aircraft Wake Vortex State-of-the-Art & Research Needs, Kapitel 4.2 Airborne Systems
Aircraft Wake Vortex State-of-the-Art & Research Needs
How plate lines influence the hazard perception of pilots during wake encounters
Development of an energy-based speed envelope for increased glideslope angles
Assessment of Energy-Efficient Approaches with Increased Glideslope Angles
Aspects of yaw control design of an aircraft with distributed electric propulsion
Aspects of yaw control design of an aircraft with distributed electric propulsion
Assessment of Aircraft Separation Reduction Potential for Arrivals Facilitated by Plate Lines
Plate lines to enhance wake vortex decay for reduced separations between landing aircraft