Development of a variable camber leading edge device design methodology

Collection of Technical Papers - AIAA 5th ATIO and the AIAA 16th Lighter-than-Air Systems Technology Conference and Balloon Systems Conference

Volumn 1, Issue , 2005, Pages 516-528

  Lajux, Vincent ^a,b   Fielding, John P ^a,b  

^a CRANFIELD UNIVERSITY   (United Kingdom)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CFD SIMULATION; LEADING EDGE (LE) DEVICES; VARIABLE CAMBER (VC);

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; ESTIMATION; PRODUCT DESIGN; WINGS;

AERODYNAMICS;

EID: 33644547998     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Fielding, J.P. (2000), 'Design investigation of variable- camber flaps for high subsonic airliners', 22nd International Congress of Aeronautical Sciences (ICAS 2000), Harrogate, AIAA, Washingon. IX, pp. Paper 2000-R. 1.2.4.
2. Niu, M.C.H. (1999), Airframe structural design: practical design information and data on aircraft structures, Kommilii Press, Hong Kong.
3. Norris, G. (14 June 2005), Creating a Titan, available at: www.flightinternational.com (accessed 26 August 2005).
4. Edi. P. (1998), Investigation of the Application of Hybrid Lamlnar Flow Control and Variable Camber Wing Design for Regional Aircraft (unpublished PhD thesis), Cranfield University, Cranfield.
5. Lajux, V. and Fielding, J.P. (2004), 'Development of the "SYNAMEC" a Design Tool for Aeronautical Mechanism applied to Leading Edge devices', 24th International Congress of Aeronautical Sciences (ICAS 2004), Yokohama, Japan. ICAS, pp. ICAS 2004-7.7.R.
6. Ammoo, M.S. (2001), Development of a Design Methodology for Transport Aircraft Variable Camber Flaps Suitable for Cruise and Low-speed Operations (unpublished PhD thesis), Cranfield University, Cranfield.