11   Artículos

 
en línea
Tomasz Goetzendorf-Grabowski and Agnieszka Kwiek    
The article presents a study on the influence of aerodynamic model fidelity on dynamic characteristics. The Simulation and Dynamic Stability Analysis (SDSA) package was used to calculate the dynamic characteristics, using both eigenvalues (linearized mod... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Zinnyrah Methal, Ahmad Syahin Abu Talib, Mohd Supian Abu Bakar, Mohd Rosdzimin Abdul Rahman, Mohamad Syafiq Sulaiman and Mohd Rashdan Saad    
This present study investigated the potential of passive flow control to reduce induced drag by using a micro-vortex generator (MVG) at a backward-facing step (BFS) location. A wing-in-ground (WIG) craft is a fast watercraft that resembles a dynamically ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Álvaro Muñoz and Pablo García-Fogeda    
In this paper, a unified method for the computation of the unsteady aerodynamic forces in the Laplace domain for a wing section in subsonic, sonic and supersonic potential flows is presented. The subsonic solution is a new development based on the pressu... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Marco Berci    
Enhanced approximate expressions for the incipient indicial lift of thin wings in subsonic potential flow are presented in this study, featuring explicit analytical corrections for the unsteady downwash. Lifting-line and acoustic-wave theories form the b... ver más
Revista: Acoustics    Formato: Electrónico

 
en línea
Carlos Carbajosa, Alejandro Martinez-Cava, Eusebio Valero and Guillermo Paniagua    
As high-pressure-turbines operate at extreme temperature conditions, base bleed can be applied at the trailing edge of the airfoils, enhancing the thermal protection along the trailing edge surface, but also disrupting the trailing edge flow and altering... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Ye Chen, Zhongxi Hou, Xiaolong Deng, Zheng Guo, Shuai Shao and Boting Xu    
The lift of an aircraft can be effectively enhanced by circulation control (CC) technology at subsonic speeds, but the efficiency at transonic speeds is greatly decreased. The underlying mechanism of this phenomenon is not fully understood. In this study... ver más
Revista: Aerospace    Formato: Electrónico

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