Fuselage shape automatic optimization with geometric constraints using a CAD based process

Collection of Technical Papers - 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

Volumn 1, Issue , 2006, Pages 445-456

  Danmas, Laurent ^a   Dinh, Quang ^a   Kleinveld, Steven ^a   Rogé, Gilbert ^a  

^a Dassault Aviation   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER AIDED DESIGN; DRAG; FINITE VOLUME METHOD; JET AIRCRAFT; NOISE ABATEMENT; STRUCTURAL OPTIMIZATION; SUPERSONIC AIRCRAFT;

EULER SHAPE OPTIMIZATION; GRADIENT BASED OPTIMIZERS; PITCHING MOMENT; SONIC BOOM REDUCTION;

FUSELAGES;

EID: 33846523035     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

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3. Q.V. Dinh, G. Rogé, C. Sevin and B. Stoufflet, "Shape Optimisation in Computational Fluid Dynamics", European Journal of Finite Elements, Vol.5, pp 569-594, Hermes, 1996.
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6. C. L. Thomas. Extrapolation of sonic boom pressure signatures by the waveform parameter method, NASA TN D-6832, June 1972.