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Volumn , Issue , 2001, Pages

Multi-criteria design optimization of two-dimensional supersonic inlet

Author keywords

[No Author keywords available]

Indexed keywords

AIR BREATHING MISSILES; MIXED COMPRESSIONS; MULTI-CRITERIA DESIGN OPTIMIZATION; OBJECTIVE FUNCTIONS; RUTGERS UNIVERSITY; SUBSONIC/SUPERSONIC FLOW; SUPERSONIC INLETS; TOTAL PRESSURE RECOVERY COEFFICIENT;

EID: 84897899699     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (14)
  • 3
    • 0032208514 scopus 로고    scopus 로고
    • Automated Optimal Design of Two Dimensional Supersonic Missile Inlets
    • M. Blaize, D. Knight and K. Rasheed. Automated Optimal Design of Two Dimensional Supersonic Missile Inlets. AIAA Journal of Propulsion and Power, Vol. 14, No. 6, pp. 890-898, 1998.
    • (1998) AIAA Journal of Propulsion and Power , vol.14 , Issue.6 , pp. 890-898
    • Blaize, M.1    Knight, D.2    Rasheed, K.3
  • 9
    • 0038188536 scopus 로고    scopus 로고
    • Application of Genetic Algorithms to High Speed Air Intake Design
    • Von Karman Institute for Fluid Dynamics, May 15-19
    • D. Knight. Application of Genetic Algorithms to High Speed Air Intake Design. Genetic Algorithms for Optimisation in Aeronautics and Turbomachinery Von Karman Institute for Fluid Dynamics, May 15-19, 2000.
    • (2000) Genetic Algorithms For Optimisation In Aeronautics and Turbomachinery
    • Knight, D.1
  • 13


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.