Use of genetic and evolutionary algorithms for aircraft conceptual design optimization

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Raymer, Daniel P ^a  

^a Conceptual Research Corporation ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ASPECT RATIO; CONCEPTUAL DESIGN; STRESS ANALYSIS;

AIRBUS A321; AIRCRAFT CONCEPTUAL DESIGNS; COMMERCIAL AIRCRAFT; CONCEPTUAL DESIGN PHASE; DESIGN PARAMETERS; EVOLUTIONARY METHOD; WING LOADING;

EVOLUTIONARY ALGORITHMS;

EID: 85087595172     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-552     Document Type: Conference Paper

References (5)

1. Raymcr. D., Enhancing Aircraft Conceptual Design using Multidisciplinary Optimization, Ph. D. Thesis, Swedish Royal Institute of Technology, Stockholm, Sweden, 2002.
2. Raymer, D., AIRCRAFT DESIGN: A Conceptual Approach, American Institute of Aeronautics and Astronautics, Washington, D. C., Third Edition 1999.
3. Raymer, D., "Multivariable Aircraft Optimization on a Personal Computer, " SAE/AIAA Paper 9965609, World Aviation Congress, 24 Oct. 1996.
4. Taylor, J., Jane's All the World Aircraft, Jane's, London, UK, (1976, 1992, 2000).
5. Raymer, D., "Vehicle Scaling Laws For Multidisciplinary Optimization, " AIAA Paper 010532, 39th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 2001.