Dynamic taxi, take-off and landing roll analyses for large business jet aircraft

被引：0

作者：

Freundt, D ^{[1
]}

McKissack, DR ^{[1
]}

Hanson, LC ^{[1
]}

Brodman, H ^{[1
]}

机构：

[1] Gulfstream Aerosp Corp, Loads & Dynam, Savannah, GA 31402 USA

来源：

COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3 | 2000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：

The FAA/JAA draft Advisory Circular (AC) pertaining to taxi, take-off, and landing roll design loads identifies dynamic analyses using random runway and tuned bump ground profiles. The large business jet model used to evaluate the requirements of the AC is comprised of experimentally validated landing gear and airframe models, which are mated in DADS(R), a commercially available non-linear dynamics software package. The results presented from this study focus on landing gear ground reactions, with secondary areas of interest that include the fuselage, wing, and nacelle loads. In addition, factors impacting simulation runtimes will be addressed.

引用

页码：1177 / 1187

页数：3

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