Fatigue Loads and Spectrum Generation for Tactical Aircraft

被引：0

作者：

Haudrich, Darin P. ^{[1
]}

Grant, Jarrod R. ^{[1
]}

Clark, Stephen F. ^{[1
]}

Nierling, Jonathan ^{[2
]}

机构：

[1] Boeing Co, Boeing Def Syst, St Louis, MO 63166 USA

[2] Boeing Co, Boeing Global Serv, St Louis, MO 63166 USA

来源：

AIAA SCITECH 2024 FORUM | 2024年

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents the current state of the art creating fatigue loads and spectrum generation for tactical aircraft at the Boeing Company - Air Dominance Division. The paper will provide examples and discussion on all aspects of the loading conditions and data delivery types for incorporation into the fatigue spectrum. Spectrum generation methodologies will be presented and discussion into the various impacts in Durability and Damage Tolerance (DaDT) analysis are provided. Considerations depending on platform mission, legacy data impacts, and customer requirements are presented.

引用

页数：12

共 12 条

[1]

[Anonymous], 1998, JSSG 2006 DEP DEF JO

[2]

[Anonymous], 1993, MIL A 8863C AIRPLANC

[3]

[Anonymous], 2019, MIL HDBK 530 1 DEP D, V1

[4]

[Anonymous], 2014, MIL HDBK 516C DEP DE

[5]

Burnham J, 1995, 36 STRUCT STRUCT DYN

[6]

Ellis Robert, 2018, 20183515 AIAA

[7]

Grover Horace J., 1966, 011A13 NAVAIR

[8]

Hoblit F., 1988, GUST LOADS AIRCRAFT

[9]

Peterson R.E., 1950, ASTM Bulletin, V164, P50

[10] Engineering time: Inventing the quartz wristwatch [J].

Stephens, CE .

PROCEEDINGS OF THE 2001 IEEE INTERNATIONAL FREQUENCY CONTROL SYMPOSIUM & PDA EXHIBITION, 2001, :2-3

← 1 2 →