A New Perspective on Battery-Electric Aviation, Part II: Conceptual Design of a 90-Seater

A New Perspective on Battery-Electric Aviation, Part I: Reassessment of Achievable Range

Distributed Hybrid-Electric Propulsion Benefits for Span-Limited Aircraft

Time-dependent reliability assessment of existing concrete bridges with varying knowledge levels by proof load testing

Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft

Proof Load Testing Method by the American Association of State Highway and Transportation Officials and Suggestions for Improvement

Proof load testing method by AASHTO and suggestions for improvement

Hybrid-Electric Aircraft with Over-the-Wing Distributed Propulsion: Aerodynamic Performance and Conceptual Design

Cross-Validation of Hybrid-Electric Aircraft Sizing Methods

Reliability assessment of existing reinforced concrete bridges and viaducts through proof load testing

Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft

Aerodynamic Performance and Static Stability Characteristics of Aircraft with Tail-Mounted Propellers

Experimental Investigation of Over-the-Wing Propeller–Boundary-Layer Interaction

Numerical Investigation of Propeller–Flap Interaction in Inclined Over-the-Wing Distributed-Propulsion Systems

Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight

An Overview of the Conceptual Design Studies of Hybrid Electric Propulsion Air Vehicles in the Frame of Clean Sky 2 Large Passenger Aircraft

Engineering method to estimate the blade loading of propellers in nonuniform flow

Range equation for hybrid-electric aircraft with constant power split

Aerodynamic Performance and Interaction Effects of Circular and Square Ducted Propellers

Synthesis of Aero-Propulsive Interaction Studies Applied to Conceptual Hybrid-Electric Aircraft Design