Fuel sensitivity analyses for active drag reduction systems

Aeronautical Journal

Volumn 108, Issue 1082, 2004, Pages 215-221

  Young, T M ^a  

^a UNIVERSITY OF LIMERICK   (Ireland)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; FLOW CONTROL; FUEL CONSUMPTION; FUEL ECONOMY; LAMINAR FLOW; MATHEMATICAL MODELS; TEMPERATURE CONTROL;

DRAG COEFFICIENT; FUEL SAVINGS; MICROELECTROMECHANICAL SYSTEMS; MULTI-VARIATE OPTIMIZATION;

AIRCRAFT FUELS;

EID: 2542449145     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000000129     Document Type: Article

References (9)

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3. Boeing. High reynolds number hybrid laminar flow control (HLFC) flight experiment, NASA CR-1999-209325/CR-1999-209326, Boeing Commercial Airplane Group, April 1999.
4. SCHRAUF, G. and KÜHN, W. Future needs and laminar flow technology, Fourth Community Aeronautical Days Conference, Hamburg, 29-31 January 2001, Proceedings in Air & Space Europe, 3, (3/4), pp 98-100.
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6. YOUNG, T.M. Investigations into the Operational Effectiveness of Hybrid Laminar Flow Control Aircraft, PhD Thesis, October 2002, Supervisor: J.P. Fielding, College of Aeronautics, Cranfield University.
7. SHUSTROV, Y.M. 'Starting mass' - a complex criterion of quality for aircraft on-board systems, J Aircr Design, 1998, 1, pp 193-203.
8. Cranfield University. Analysis of the fuel penalties of airframe systems, Lecture note DAeT 95122, College of Aeronautics, Cranfield University. (Unpublished).
9. LE CLAIRE, R. Energy management fuel weight penalty of aircraft systems, BAe-KSE-R-GEN-1334. BAe Kingston-Upon-Thames, June 1986. (Cited in Cranfield University lecture note DAeT 95122).