Low cost structural concept for composite trailing edge flap

Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials

Volumn 12, Issue 4, 2004, Pages 281-300

  Hirose, Y ^a,b   Taki, T ^a   Mizusaki, Y ^a   Fujita, T ^a  

^a KAWASAKI HEAVY INDUSTRIES LTD   (Japan)

^b KHI   (Japan)

Author keywords

Composite structure; Low cost design; Low cost fabrication; Trailing edge flap

Indexed keywords

AERODYNAMICS; COMPOSITE MATERIALS; COMPUTATIONAL FLUID DYNAMICS; COSTS; DURABILITY; HONEYCOMB STRUCTURES; LAMINATES; SANDWICH STRUCTURES; STRUCTURAL DESIGN;

JAPAN AIRCRAFT DEVELOPMENT CORPORATION (JADC); LOW COST DESIGN; LOW COST FABRICATION; TRAILING EDGE FLAP;

COMPOSITE STRUCTURES;

EID: 2342508484     PISSN: 09243046     EISSN: None     Source Type: Journal    
DOI: 10.1163/156855103322986565     Document Type: Article

References (2)

1. Y. Hirose, S. Bando, H. Masaeda and N. Tsuda, Application studies of a new graphite/epoxy material for the vertical fin of a commercial transport aircraft, in: Proc. Third Japan-US Conf. Compos. Mater., pp. 683-691 (1986).
2. S. Sonoda, KR19168, YSX Flap Aerodynamic Design Report, Japan Aircraft Development Corporation (JADC) (1996).