Towards More Efficient Electric Propulsion UAV Systems Using Boundary Layer Ingestion
The implementation of distributed propulsion and boundary layer ingestion for unmanned aerial vehicles represents various challenges for the design of embedded ducts in blended wing body configurations. This work explores the conceptual design and evaluation of DP configurations with BLI. The aerody...
Main Authors: | Jonathan Arias, Francisco Martinez, Edgar Cando, Esteban Valencia |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-11-01
|
Series: | Drones |
Subjects: | |
Online Access: | https://www.mdpi.com/2504-446X/7/12/686 |
Similar Items
-
Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan
by: Alexander C. Smith, et al.
Published: (2019-04-01) -
Development of a Multi-Segment Parallel Compressor Model for a Boundary Layer Ingesting Fuselage Fan Stage
by: Jonas Voigt, et al.
Published: (2021-09-01) -
Influences of distributed propulsion system parameters on aerodynamic characteristics of a BLI-BWB UAV
Published: (2021-02-01) -
The preliminary design of ducted fan for VTOL UAV /
by: 327689 Lee, Boon Chieh, et al.
Published: (2007) -
Proof of Concept Study for Fuselage Boundary Layer Ingesting Propulsion
by: Arne Seitz, et al.
Published: (2021-01-01)