26   Artículos

 
en línea
Yuan Wei, Renliang Chen, Ye Yuan and Luofeng Wang    
This study assesses the influence of engine dynamic characteristics on helicopter handling quality during hover and low-speed forward flight. First, we construct the helicopter?engine coupling model (HECM) based on the power-matching relationship between... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lixin Wang, Chang Lu, Tao Jin, Hailiang Liu and Ting Yue    
Using a nonlinear pilot-induced oscillation prediction method based on digital virtual flight simulation calculations, digital experiments on predicting lateral-directional nonlinear pilot-induced oscillations due to landing configuration switching of fl... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Frédéric Moëns    
A multidisciplinary design analysis and optimization process is developed at ONERA for the design of tube and wing and blended wing?body aircraft configurations. This process is composed of different disciplinary modules (geometry, propulsion, aerodynami... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Johan Feldwisch and Martin Bauer    
With the progress of high-performance computing, computationally expensive high-fidelity methods can be applied early in the design process of an aircraft. This enables Computational Fluid Dynamics (CFD) for the assesment of flight performance, handling ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ye Yuan, Douglas Thomson and David Anderson    
The tiltrotor has unique flight dynamics due to the aerodynamic interference characteristics. Multiple aerodynamics calculation approaches, such as the CFD method, are utilised to characterise this feature. The calculation process is usually time-consumi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Omkar Halbe and Manfred Hajek    
This paper synthesizes a continuous, multivariable, finite-time-convergent, super-twisting attitude and rate controller for rotorcraft with the objective of providing desired handling qualities and robustness characteristics. A sliding manifold is define... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mohsen Rostami, Julian Bardin, Daniel Neufeld and Joon Chung    
In considering aircraft design, it is very important to effectively size the tail configuration for stability and control. Multidisciplinary design optimization (MDO) focuses on the use of numerical optimization in the design of systems with multiple sub... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Peyman Alizadeh, Tim Dumonceaux, Lope G. Tabil, Edmund Mupondwa, Majid Soleimani and Duncan Cree    
The current study explores steam explosion pre-treatment of wood sawdust to develop high-quality biofuel pellets. In order to determine optimized conditions (temperature and residence time) for steam-treated biomass, seven test responses were chosen, inc... ver más
Revista: Clean Technologies    Formato: Electrónico

 
en línea
Luís M. B. C. Campos and Joaquim M. G. Marques    
The coupling of the longitudinal and lateral stability modes of an aeroplane is considered in two cases: (i) weak coupling, when the changes in the frequency and damping of the phugoid, short period, dutch roll, and helical modes are small, i.e., the squ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Clayton Humphreys-Jennings, Ilias Lappas and Dragos Mihai Sovar    
The Blended Wing Body (BWB) configuration is considered to have the potential of providing significant advantages when compared to conventional aircraft designs. At the same time, numerous studies have reported that technical challenges exist in many are... ver más
Revista: Aerospace    Formato: Electrónico

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