Verification of a chamberless HLFC design with an outer skin of variable porosity
Energy-optimal guidance of a battery-electrically driven airplane
Quieter and Greener rotorcraft: concurrent aerodynamic and acoustic optimization
Towards higher aerodynamic efficiency of propeller-driven aircraft with distributed propulsion
PARE preliminary analysis of ACARE FlightPath 2050 environmental impact goals
Comparison and evaluation of blade element methods against RANS simulations and test data
Application of VR technology in the aircraft cabin design process
Numerical investigation of tangential blowing over the rudder of a vertical tailplane
Design of a synthetic jet actuator for flow separation control
Case study on the environmental impact and efficiency of travel
Integration aspects of the collaborative aero-structural design of an unmanned aerial vehicle
Exact solution for thermal–mechanical post-buckling of functionally graded micro-beams
Simulation of transonic buffet with an automated zonal DES approach
Parametric whirl flutter study using different modelling approaches
Analyzing door-to-door travel times through mobile phone data
Numerical investigation of the effects of fuselage upsweep in a propulsive fuselage concept
A multi-channel H∞ preview control approach to load alleviation design for flexible aircraft
Assessment of the efficiency of an active winglet concept for a long-range aircraft
Technology selection for holistic analysis of hybrid-electric commuter aircraft
Design and flight test of a linear parameter varying flight controller
Ducted fans for hybrid electric propulsion of small aircraft
Analysis of rotorcraft wind turbine wake encounters using piloted simulation
How future aircraft can benefit from a steerable main landing gear for crosswind operations
Progress in the airworthiness technology of civil aero-engine
Development of a quasi-linear parameter varying model for a tiltrotor aircraft
Aeroelastic behaviour of a wing with over-the-wing mounted UHBR engine
The use of the Open-Loop Onset Point (OLOP) to predict rotorcraft pilot-induced oscillations