Outcomes of Nonlinear Static Aeroelasticity for Wing Stress and Buckling

被引：0

作者：

Verri, Angelo Antonio ^{[1
]}

de Silva Bussamra, Flavio Luiz ^{[2
]}

Cesnik, Carlos E. S. ^{[3
]}

de Melo, Felipe Buarque Cordeiro ^{[4
,5
]}

机构：

[1] EMBRAER S A, Loads & Aeroelast, BR-12227901 Sao Jose Dos Campos, SP, Brazil

[2] Technol Inst Aeronaut, Aerosp Struct Dept, BR-12228900 Sao Jose Dos Campos, SP, Brazil

[3] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA

[4] Embraer S A, Loads & Aeroelast, BR-12227901 Sao Jose Dos Campos, SP, Brazil

[5] Technol Inst Aeronaut, Postgrad Course, BR-12228900 Sao Jose Dos Campos, SP, Brazil

来源：

JOURNAL OF AIRCRAFT | 2025年

关键词：

Buckling Criterion; Nonlinear Static Aeroelasticity; Fluid Structure Interaction; Geometrically Nonlinear Analysis; Aircraft Wing Design; Aircraft Components and Structure; Aeronautics; Nonlinear Aeroelasticity; Geometric Nonlinear Analysis; Embraer Aircrafts; AIRCRAFT; DESIGN;

D O I：

10.2514/1.C037829

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页数：5