Modelling and design of wing tip devices at various flight conditions using a databased aerodynamic prediction tool{star, open}{star, open}This article was presented at the German Aerospace Congress 2004.

Aerospace Science and Technology

Volumn 10, Issue 8, 2006, Pages 668-678

  Büscher, Alexander ^a   Radespiel, Rolf ^a   Streit, Thomas ^b  

^a TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Drag due to lift; Induced drag; M DAW; Nonplanar wing; Winglet

Indexed keywords

COMPUTER SIMULATION; DATABASE SYSTEMS; DRAG; FLIGHT DYNAMICS; MACHINE DESIGN; TECHNICAL PRESENTATIONS;

INDUCED DRAG; LIFT AND DRAG COMPONENT ANALYSIS (LIDCA); M-DAW; NONPLANAR WING;

WINGS;

EID: 33751187895     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2006.03.001     Document Type: Article

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