Reliability based design optimization of a solid rocket motor using surrogate models

Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Volumn 8, Issue , 2007, Pages 8126-8144

  Kuran, Bayindir ^a,b  

^a SCIENTIFIC AND TECHNOLOGICAL RESEARCH COUNCIL OF TURKEY   (Turkey)

^b Systems and Specialty Engineering Division   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

FAILURE ANALYSIS; MATHEMATICAL MODELS; NEURAL NETWORKS; OPTIMIZATION; RELIABILITY ANALYSIS; SOLID PROPELLANTS;

CENTRAL COMPOSITE DESIGN (CCD); FIRST ORDER RELIABILITY METHOD (FORM); LATIN HYPERCUBE SAMPLING (LHS) METHODS; UNIFORM SAMPLING (US);

ROCKET ENGINES;

EID: 36749085118     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-5825     Document Type: Conference Paper

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