Results 1 to 10 of about 124 (100)

Integration of the athena vortex lattice aerodynamic analysis software into the multivariate design synthesis of a blended wing body aircraft [PDF]

open access: yesHeliyon, 2023
This paper describes the process of integrating the Athena Vortex Lattice aerodynamics solver into a conceptual design environment for the multivariate design synthesis and optimisation of a Blended Wing Body (BWB) Aircraft.
Paul Okonkwo, Paul Jemitola
doaj   +4 more sources

Design, Computational Aerodynamic, Aerostructural, and Control Stability Investigations of VTOL-Configured Hybrid Blended Wing Body-Based Unmanned Aerial Vehicle for Intruder Inspections

open access: yesInternational Journal of Aerospace Engineering, 2023
Unmanned aerial vehicles (UAVs) are gaining in popularity and sophistication in today’s modern world. UAVs are now available in a wide range of configurations. A UAV’s many applications include aerial photography and videography and target tracking.
Vijayanandh Raja   +9 more
doaj   +2 more sources

Design Improvement of a BWB Aerodynamic Performance at Cruise and Take-Off Speeds

open access: yesInternational Journal of Aerospace Engineering, 2022
As a high-performance aircraft, BWB (blended wing body) has attracted the attention of many countries around the world. A 300-seat BWB design is proposed by the Airplane Concept Design Institute of Northwestern Polytechnical University, which is also ...
Gang Yu, Yuling Duan
doaj   +2 more sources

Blended Wing Body Thrust Reverser Cascade Feasibility Evaluation Through CFD

open access: yesIEEE Access, 2019
Airplane thrust reverser could significantly reduce the landing distance of a conventional civil turbofan. Control of the thrust reverser can be performed by a hydraulic and/or electric system.
Yu Gang   +3 more
doaj   +3 more sources

Conceptual Design, Flying, and Handling Qualities Assessment of a Blended Wing Body (BWB) Aircraft by Using an Engineering Flight Simulator

open access: yesAerospace, 2020
The Blended Wing Body (BWB) configuration is considered to have the potential of providing significant advantages when compared to conventional aircraft designs.
Clayton Humphreys-Jennings   +2 more
doaj   +3 more sources

Comprehensive Evaluation and Trade‐Off of Top‐Level Requirements for BWB UAVs

open access: yesEngineering Reports
To enhance the rationality of top‐level requirement development for Blended Wing Body (BWB) Unmanned Aerial Vehicles (UAVs), a top‐level requirement trade‐off process is established to transform the requirement trade‐off into an evaluation and ...
Xinshi Suo   +3 more
doaj   +2 more sources

Flow Field Investigation of a Blended Wing Body in Low Speeds [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2023
With the advancement in the modern transport system, it has become imperative to achieve larger aircraft volume at minimum cost wherein aerodynamics plays a major role.
A. Arora, S. Das, P. Kumar
doaj   +1 more source

Design and analysis pertaining to the aerodynamic and stability characteristics of a hybrid wing-body cargo aircraft [PDF]

open access: yesINCAS Bulletin, 2017
Recent trends in aircraft design research have resulted in development of many unconventional configurations mostly aimed at improving aerodynamic efficiency. The blended wing body (BWB) is one such configuration that holds potential in this regard.
Ishaan PRAKASH, Prithwish MUKHERJEE
doaj   +1 more source

Numerical investigation for influence of powered effect on aerodynamic performance of BWB takeoff configuration

open access: yesMathematical and Computer Modelling of Dynamical Systems, 2023
The influence of the powered effect on the aerodynamic performance of the blended-wing-body (BWB) takeoff configuration is analysed in this study by solving the three-dimensional Reynolds-averaged Navier–Stokes equation on a multiblock structured grid ...
Gang Yu, Dong Li, Yuling Duan
doaj   +1 more source

Stability study and flight simulation of a blended-wing-body UAV [PDF]

open access: yesMATEC Web of Conferences, 2019
This article is a product of the design process of a Blended-Wing- Body Unmanned Aerial Vehicle (BWB UAV). The BWB geometry blends the wing and the fuselage so that the fuselage also contributes in lift generation.
Dimopoulos Thomas   +2 more
doaj   +1 more source

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