Results 21 to 30 of about 1,065 (263)

Study on Cruise Drag Characteristics of Low Drag Normal Layout Civil Aircraft

open access: yesXibei Gongye Daxue Xuebao, 2020
This paper focus on the wing shape related drag reduction measures of normal layout civil aircraft, through the drag reduction to improve the aircraft performance.

doaj   +1 more source

Aerodynamic analysis of potential flow over blended-wing-body (BWB) aircraft [PDF]

open access: yesمجله مدل سازی در مهندسی, 2017
In this investigation, a numerical method based on potential flow for aerodynamic analysis of BWB aircrafts has been developed. At first, results of this method are validated with experimental data and then, three current BWB planforms have been chosen ...
Mohammad Hasan Djavareshkian   +1 more
doaj   +1 more source

On Noise Assessment for Blended Wing Body Aircraft [PDF]

open access: yes52nd Aerospace Sciences Meeting, 2014
A system noise study is presented for the blended-wing-body (BWB) aircraft configured with advanced technologies that are projected to be available in the 2025 timeframe of the NASA N+2 definition. This system noise assessment shows that the noise levels of the baseline configuration, measured by the cumulative Effective Perceived Noise Level (EPNL ...
Yueping Guo   +2 more
openaire   +1 more source

Analysis on energy consumption of blended-wing-body underwater glider

open access: yesInternational Journal of Advanced Robotic Systems, 2020
As a new type of underwater observation platform, underwater glider is widely used in marine explorations and military surveys, and most gliders are powered by their own batteries whose capacities are limited.
Xiaoxu Du, Lianying Zhang
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

An alternative approach to induced drag reduction

open access: yesAviation, 2021
Induced drag constitutes approximately 40% of the total drag of subsonic civil transport aircraft at cruise conditions. Various types of winglets and several non-planar concepts, such as the C-wing, the joined wings, and the box plane, have been proposed
Nikolaos Kehayas
doaj   +1 more source

Handling Qualities of a Blended Wing Body Aircraft [PDF]

open access: yesAIAA Atmospheric Flight Mechanics Conference, 2011
The blended wing body (BWB) is a tailless aircraft with the potential to use 27% less fuel than a conventional aircraft with the same passenger capacity and range. The primary purpose of the current study was to determine the handling qualities of the BWB, using piloted-handling trials in a moving-base simulator.
Tim Peterson, Peter Grant
openaire   +1 more source

Shape optimization of blended-wing-body underwater glider by using gliding range as the optimization target

open access: yesInternational Journal of Naval Architecture and Ocean Engineering, 2017
Blended-Wing-Body Underwater Glider (BWBUG), which has excellent hydrodynamic performance, is a new kind of underwater glider in recent years. In the shape optimization of BWBUG, the lift to drag ratio is often used as the optimization target.
Chunya Sun   +3 more
doaj   +1 more source

Discrete optimization design for cabin-skeleton coupling structure of blended-wing-body underwater glider

open access: yesZhongguo Jianchuan Yanjiu, 2021
ObjectivesThe cabin-skeleton coupling structure of a blended-wing-body underwater glider is optimized using a data-driven discrete optimization concept.MethodsFirst, a Kriging-assisted discrete global optimization algorithm (KDGO) is proposed for ...
Huachao DONG, Peng WANG, Yijin ZHANG
doaj   +1 more source

Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System

open access: yesInternational 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
doaj   +1 more source

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