Generic process for air vehicle concept design and assessment

AIAA Paper

Volumn , Issue , 2004, Pages 11418-11427

  Doherty, John J ^a,b   McParlin, Stephen C ^a,c  

^a QINETIQ   (United Kingdom)

^b Aerodynamic Technology   (United Kingdom)

^c Aerodynamic Technology

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; COMPUTER AIDED DESIGN; DATABASE SYSTEMS; FUSELAGES; KNOWLEDGE BASED SYSTEMS; MATHEMATICAL MODELS; OPERATIONS RESEARCH; OPTIMIZATION; WINGS;

AIR VEHICLES; MASS ESTIMATION METHODS; OPERATIONAL ANALYSIS; PARAMETRIC MODELS;

AERODYNAMICS;

EID: 2942716952     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-895     Document Type: Conference Paper

References (7)

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2. Crawford C. A. and Simm S. E., "Conceptual design and optimisation of modern combat aircraft", in "Aerodynamic design and optimisation of flight vehicles in a concurrent multi-disciplinary environment", NATO RTO Symposium, Ottawa, Canada, 18-21 October 1999.
3. Skrobanski J. J., "Optimisation subject to nonlinear constraints", PhD. Thesis, University of London, 1986.
4. Lovell D. A. and Doherty J. J., "Aerodynamic design of aerofoils and wings using a constrained optimisation method", Paper ICAS-94-2.1.2, International Congress of the Aerospace Sciences, Anaheim, California, 1994.
5. McParlin S. C., Doherty J. J. and Wood S. E., "Validation of a multi-block Euler method for supersonic flows about complex aircraft configurations", Royal Aeronautical Society Conference on "Recent developments and applications in aeronautical CFD", Bristol, September 1993.
6. st ASME, Reno, Nevada, 6-9 Jan 2003.
7. Fenwick S. V. and Harris J. ap C., "The application of Pareto Frontier methods in the multi-disciplinary wing design of a generic modern military delta aircraft", in "Aerodynamic design and optimisation of flight vehicles in a concurrent multi-disciplinary environment", NATO RTO Symposium, Ottawa, Canada, 18-21 October 1999.