Acceso al sitio web del Consejo de Políticas de Infraestructura
REVISTA
Aerospace

   
Redirigiendo al acceso original de articulo en 19 segundos...
Inicio  /  Aerospace  /  Vol: 5 Núm: 2 Par: June (2018)  /  Artículo
ARTÍCULO
TITULO

Aircraft Geometry and Meshing with Common Language Schema CPACS for Variable-Fidelity MDO Applications

Mengmeng Zhang    
Aidan Jungo    
Alessandro Augusto Gastaldi and Tomas Melin    

Resumen

This paper discusses multi-fidelity aircraft geometry modeling and meshing with the common language schema CPACS. The CPACS interfaces are described, and examples of variable fidelity aerodynamic analysis results applied to the reference aircraft are presented. Finally, we discuss three control surface deflection models for Euler computation.

Palabras claves

PÁGINAS

 Artículos similares

       
 
Daniele Granata, Alberto Savino and Alex Zanotti    
The present study aimed to investigate the capability of mid-fidelity aerodynamic solvers in performing a preliminary evaluation of the static and dynamic stability derivatives of aircraft configurations in their design phase. In this work, the mid-fidel... ver más
Revista: Aerospace

 
Nicholas F. Giannelis, Tamas Bykerk and Gareth A. Vio    
This paper introduces a generic model for the study of aerodynamic behaviour relevant to fifth-generation high-performance aircraft. The model design is presented, outlining simplifications made to retain the key features of modern high-performance vehic... ver más
Revista: Aerospace

 
David I. Barton, Cesare A. Hall and Matthew K. Oldfield    
Contrails are responsible for a significant proportion of aviation?s climate impact. This paper uses data from the European Centre for Medium-Range Weather Forecasts to identify the altitudes and latitudes where formed contrails will not persist. This re... ver más
Revista: Aerospace

 
Yuki Kishi, Risato Yashiro and Masahiro Kanazaki    
Forward-swept wings can be expected to be lower-boom planforms with similar amount of drag as backward-swept wings because of their good lift distributions. In this study, the equivalent area distribution of a ten-seater supersonic forward-swept wing air... ver más
Revista: Aerospace

 
Ángel Antonio Rodríguez-Sevillano, María Jesús Casati-Calzada, Rafael Bardera-Mora, Javier Nieto-Centenero, Juan Carlos Matías-García and Estela Barroso-Barderas    
This paper shows a series of tools that help in the research of morphing micro air vehicles (MAVs). These tools are aimed at generating parametric CAD models of wings in a few seconds that can be used in aerodynamic studies, either via CFD directly using... ver más
Revista: Aerospace