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Aeromechanics Analysis of a Boundary Layer Ingesting Fan [PDF]
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2012 Boundary layer ingesting propulsion systems have the potential to significantly reduce fuel burn but these systems must overcome the challe nges related to aeromechanics-fan flutter stability and forced response dynamic stresses. High-fidelity computational analysis of the fan a eromechanics is integral to the ongoing effort to design a boundary layer ...
Milind Bakhle +4 more
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Aerospace, 2023 The aerodynamic design of a new aircraft concept was investigated through subsonic wind-tunnel testing using 1:28-scale powered models. The aircraft configuration integrates a box-wing layout with engines located at the rear part of the fuselage ...
Pedro D. Bravo-Mosquera +2 more
doaj +1 more source
Energies, 2022 A distributed propulsion system has the advantage of saving 5–15% fuel burn through ingesting the fuselage boundary layer of an aircraft by fan or compressor.
Tianyu Pan +4 more
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Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System
International Journal of Aerospace Engineering, 2021 A blended-wing-body aircraft has the advantages of high lift-to-drag ratio, low noise, and high economy compared with traditional aircraft. It is currently a solution with great potential to become a future civilian passenger aircraft.
Yuan Jia, Jinye Li, Jianghao Wu
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Drones, 2022 New propulsive architectures, with high interactions with the aerodynamic performance of the platform, are an attractive option for reducing the power consumption, increasing the resilience, reducing the noise and improving the handling of fixed-wing ...
José Ramón Serrano +3 more
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Hybrid Flow Control on Boundary Layer Ingestion Inlet
Journal of Physics: Conference Series, 2021 Abstract For the boundary layer ingestion (BLI) inlet, how to control the flow is very important to improve the quality of the air flow at the outlet. In this paper, the research on the passive flow control is carried out by using rectangular straight spoiler blades, and the active flow control is carried out by using the blowing pipes ...
Yinhui Shang +3 more
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Aerospace, 2023 Present work investigates the potential of a long-range commercial blended wing body configuration powered by hydrogen combustion engines with future airframe and propulsion technologies.
Stanislav Karpuk, Yiyuan Ma, Ali Elham
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Propulsion Airframe Integration: Aerodynamic Modeling of Boundary Layer Ingestion
, 2022 "Propulsion airframe integration offers a range of benefits, while opening the realm of design options for future air-vehicle configurations. The aerodynamic complexity resulting from interaction between airframe and propulsion system, however, still ...
KOB, LUCAS LEANDER
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Control of a Supersonic Inlet in Off-Design Conditions with Plasma Actuators and Bleed
Aerospace, 2020 Supersonic inlets are a key component of present and future air-breathing propulsion systems for high-speed flight. The inlet design is challenging because of several phenomena that must be taken under control: shock waves, boundary layer separation and ...
Andrea Ferrero
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Body Force Modeling of the Aerodynamics of a Low-Speed Fan under Distorted Inflow †
International Journal of Turbomachinery, Propulsion and Power, 2019 New propulsive concepts, such as boundary layer ingestion, involve stronger interactions between the engine and its environment, and are thus more complex flows compared to classical architectures.
Emmanuel Benichou +5 more
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