Investigation of weight reduction in a thrust reverser cascade using aerodynamic and structural integration

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 2, Issue , 2003, Pages 1578-1585

  Butterfield, J ^a   Yao, H ^a   Benard, E ^a   Price, M ^a   Cooper, R ^a   Monaghan, D ^a   Armstrong, C ^a   Raghunathan, S ^a  

^a QUEEN'S UNIVERSITY BELFAST   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FINITE ELEMENT METHOD;

AERODYNAMIC SIMULATION; THRUST REVERSER CASCADE;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0042512416     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1576     Document Type: Conference Paper

References (6)

1. Asbury S. C., Yetter J. A., "Static Performance of Six Innovative Thrust Reverser Concepts for Subsonic Transport Applications", NASA/TM-2000-210300, July 2000.
2. Anon, Rolls Royce Aerospace Group, "The Jet Engine", Renault Printing Co. Ltd., Birmingham, England, Fifth Edition, 1996, pp 159-169.
3. Broede, J, "Saving Costs in Design, Manufacturing and Operation of Aero Engine Parts", The Aeronautical Journal, November 2001, pp 619-626.
4. Tindell R. H., Marconi F., Kalkhoran I., Yetter, J., "Deflection of Turbofan Exhaust Streams for Enhanced Engine/Nacelle Integration", Journal of Aircraft, Vol. 35, No 1, January-February 1998.
5. Gunston, B., "The Development of Jet and Turbine Aero Engines", Haynes Publishing, Sparkford, England. Second Edition, 1997, pp 59-62.
6. Butterfield, J. et al., "Methodologies for Structural Optimisation of a Thrust reverser Cascade Using a Multidisciplinary Approach". AIAA 41st Aerospace Sciences and Exhibit, 6-9 January, 2003, Reno Hilton, Reno, Nevada.