Results 81 to 90 of about 528 (156)

Preliminary Sizing of a Medium Range Blended Wing-Body using a Multidisciplinary Design Analysis Approach

MATEC Web of Conferences, 2018
The aviation's goal for the next decades is to drastically reduce emissions, but to achieve this goal a breakdown in aircraft design has to be considered.
Sgueglia Alessandro, Schmollgruber Peter, Benard Emmanuel, Bartoli Nathalie, Morlier Joseph   +4 more
doaj   +1 more source

Aerodynamic performance of a blended-wing-body configuration aircraft

, 2006
In recent years new configurations for large commercial transport aircraft have been investigated to meet an increasing demand in international travel, particularly between major capital cities (hubs).
Cornelis Bil (18025165), Toshihiro Ikeda (7274225)   +1 more
core  

Effective multiobjective MDO for conceptual design - An aircraft design perspective [PDF]

, 2007
Once the requirements for a new aircraft have been defined, the Conceptual design phase is launched. During this phase one or more designers have the goal of defining and investigating a number of alternative solutions.
Fantini, Paolo
core  

Synergetic Technology Evaluation of Aerodynamic and Performance-Enhancing Technologies on a Tactical BWB UAV

Drones
The current study presents a holistic technology evaluation and integration methodology for enhancing the aerodynamic efficiency and performance of a tactical, fixed-wing Blended-Wing-Body (BWB) Unmanned Aerial Vehicle (UAV) through the synergetic ...
Stavros Kapsalis, Pericles Panagiotou, Kyros Yakinthos   +2 more
doaj   +1 more source

Étude de la stabilité d'un avion BWB (Blended Wing Body) de 200 passagers [PDF]

, 2015
RÉSUMÉ: Le Blended Wing Body (BWB) est un type d'avion innovant, basé sur le concept d'aile volante. Ce nouveau type d'avion présente de nombreux avantages par rapport aux avions conventionnels : économie de carburant et réduction du poids de la ...
Legros, Clément
core  

Concept Evaluation of Radical Short–Medium-Range Aircraft with Turbo-Electric Propulsion

Aerospace
Ambitious targets for the coming decades have been set for further reductions in aviation greenhouse gas emissions. Hybrid electric propulsion (HEP) concepts offer potential for the mitigation of these aviation emissions. To investigate this potential in
W. J. Vankan, W. F. Lammen, E. Scheers, P. J. Dewitte, Sebastien Defoort   +4 more
doaj   +1 more source

Study of Modeling and Optimal Take-Off Scheme for a Novel Tilt-Rotor UAV. [PDF]

Sensors (Basel), 2022
Yu Z, Zhang J, Wang X.
europepmc   +1 more source

Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali [PDF]

, 2015
The Blended Wing-Body (BWB) aircraft is an unconventional aircraft that offers the aerodynamics performance advantages compared to the conventional aircraft.
Mohd Ali, Zurriati
core  

Computational Analysis of Liquid Hydrogen Storage Tanks for Aircraft Applications. [PDF]

Materials (Basel), 2023
Mantzaroudis VK, Theotokoglou EE.
europepmc   +1 more source

An integrated framework for static stability design of tailless BWB mini-UAVs based on XFLR5, LHS, and Gaussian Process Regression

Mechanics & Industry
Tailless blended wing body (BWB) mini-UAVs offer important aerodynamic and structural advantages, but the absence of conventional tail surfaces makes inherent static stability difficult to achieve during conceptual design.
Hakim Mohamed, Choukri Saad, Ait Ali Mohamed E.   +2 more
doaj   +1 more source