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Volumn , Issue , 2002, Pages

A comparative study of genetic algorithm and orthogonal steepest descent for aircraft multidisciplinary optimization

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84862481089     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (9)
  • 3
    • 0033893538 scopus 로고    scopus 로고
    • Conceptual Aircraft Design Based on a Multiconstraint Genetic Optimizer
    • Mar.-Apr
    • Blasi, L. et al., "Conceptual Aircraft Design Based on a Multiconstraint Genetic Optimizer", AIAA Journal of Aircraft Vol. 37 No. 2, Mar.-Apr. 2000 (page 351)
    • (2000) AIAA Journal of Aircraft , vol.37 , Issue.2 , pp. 351
    • Blasi, L.1
  • 7
    • 0003631917 scopus 로고    scopus 로고
    • American Institute of Aeronautics and Astronautics, Washington, D.C., Third Edition
    • Raymer, D., AIRCRAFT DESIGN: A Conceptual Approach, American Institute of Aeronautics and Astronautics, Washington, D.C., Third Edition 1999
    • (1999) AIRCRAFT DESIGN: A Conceptual Approach
    • Raymer, D.1
  • 9
    • 84894866520 scopus 로고    scopus 로고
    • Vehicle Scaling Laws For Multidisciplinary Optimization
    • AIAA Paper 01-0532, Reno, NV, Jan
    • Raymer, D., "Vehicle Scaling Laws For Multidisciplinary Optimization", AIAA Paper 01-0532, 39th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 2001
    • (2001) 39th AIAA Aerospace Sciences Meeting
    • Raymer, D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.