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Preliminary Assessment of a Distributed Electric Propulsion System for the SUSAN Electrofan
View Video Presentation: https://doi. org/10.2514/6.2023-1748. vid The SUSAN Electrofan is
a new hybrid electric large regional jet aircraft concept being studied by NASA that …
a new hybrid electric large regional jet aircraft concept being studied by NASA that …
Toward the Development of an Underwing Boundary Layer Ingesting Distributed Propulsion System for the SUSAN Electrofan
The SUSAN Electrofan is a new hybrid-electric regional jet aircraft being investigated by
NASA that leverages advanced propulsion technologies to reduce aviation energy usage …
NASA that leverages advanced propulsion technologies to reduce aviation energy usage …
High-Fidelity Aeropropulsive Assessment of Distributed Electric Propulsion and Boundary Layer Ingestion for the SUSAN Electrofan
The Subsonic Single Aft Engine (SUSAN) Electrofan is a new hybrid electric 180 passenger
transport aircraft being developed at NASA, which aims to achieve significant reductions in …
transport aircraft being developed at NASA, which aims to achieve significant reductions in …
Aeropropulsive Assessment of a BLI Tail-Cone Thruster Propulsion System for the NASA Common Research Model and a Transonic Truss-Braced Wing Configuration
LM Machado, T Chau, J Duensing - AIAA AVIATION FORUM AND …, 2024 - arc.aiaa.org
This paper presents an investigation into the potential benefits of a boundary layer ingestion
(BLI) aft fuselage propulsion system, or tail-cone thruster (TCT), when applied to two …
(BLI) aft fuselage propulsion system, or tail-cone thruster (TCT), when applied to two …
Wall-Modeled Large Eddy Simulations of Transonic Buffet Over a Supercritical Airfoil
A series of scale-resolving simulations of flow over the ONERA OAT15A airfoil have been
performed at an angle of attack of 3.5 degrees, just past the onset of buffet. The focus of this …
performed at an angle of attack of 3.5 degrees, just past the onset of buffet. The focus of this …
Development of 3D Flow Analysis Method for Multicopter Rotors by Combination of Blade Element Theory and Actuator Line Model
The actuator line model (ALM), which models the rotor blade as a set of points with an
external force term, and the actuator disk model (ADM), which models the rotor as a disk with …
external force term, and the actuator disk model (ADM), which models the rotor as a disk with …
Comparing Methods to Extract Sectional Angle of Attack From Blade-Resolved Rotor Simulations
The angle of attack is widely used to describe the aerodynamics of rotor blades. Models
based on lifting lines, actuator lines, and actuator disks use it as a primary variable …
based on lifting lines, actuator lines, and actuator disks use it as a primary variable …