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
收藏
页数：5
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