A FEM-Based Approach for Nonlinear Aeroelastic Trim of Highly Flexible Aircraft

Autor:	Cristina Riso, Di Vincenzo, F. G., Ritter, M., Cesnik, C. E. S., Mastroddi, F.
Rok vydání:	2017
Předmět:	Steady Horizontal Trim inertia relief Nastran SOL400 finite element method fluid-structure interaction Very Flexible Aircraft highly flexible aircraft nonlinear aeroelastic trim Vortex-Lattice
Zdroj:	Scopus-Elsevier
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::4c1c09a21fa4af0b366e5da1dc01f130 https://elib.dlr.de/118373/ Zobrazit plný text záznamu