Static Aeroelastic Analysis of an Aircraft Wind-Tunnel Model by Means of Modal RBF Mesh Updating-Reference-Cited by-同舟云学术

Static Aeroelastic Analysis of an Aircraft Wind-Tunnel Model by Means of Modal RBF Mesh Updating

Published:2016-11 Issue:6 Volume:29 Page:04016061
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Biancolini Marco Evangelos¹,Cella Ubaldo²,Groth Corrado³,Genta Massimiliano⁴

Affiliation:

1. Professor, Dept. of Enterprise Engineering, Univ. of Rome “Tor Vergata”, via Politecnico 1, 00133 Rome, Italy (corresponding author).

2. Senior Research Engineer, Design Methods, Viale Regina Elena 207, 98121 Messina, Italy.

3. Ph.D. Student, Dept. of Enterprise Engineering, Univ. of Rome “Tor Vergata”, via Politecnico 1, 00133 Rome, Italy.

4. Research Engineer, Dept. of R&D, Piaggio Aerospace, Viale Generale Disegna 1, Villanova d’Albenga, 17038 Savona, Italia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000627

Reference24 articles.

1. ANSYS 15.0 [Computer software]. ANSYS Canonsburg PA.

2. Mesh morphing accelerates design optimization;Biancolini M. E.;ANSYS Adv. J.,2010

3. Biancolini M. E. (2011). “Fluid structure interaction (FSI) with RBF morph: A generic formula 1 front end.” EnginSoft Int. Conf. 2011—CAE Technologies for Industry Enginsoft Spa Trento Italy.

4. Mesh Morphing and Smoothing by Means of Radial Basis Functions (RBF)

5. Biancolini M. E. and Cella U. (2010). “An advanced RBF Morph application: Coupled CFD-CSM aeroelastic analysis of a full aircraft model and comparison to experimental data.” Low Carbon Vehicles: 8th MIRA Int. Vehicle Aerodynamics Conf. MIRA U.K. 490.

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