Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps

Aeronautical Journal

Volumn 111, Issue 1117, 2007, Pages 165-174

  Wong, W S ^a   Le Molgne, A ^a   Qin, N ^a  

^a UNIVERSITY OF SHEFFIELD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

GEOMETRY; GRID COMPUTING; OPTIMIZATION; SHOCK ABSORBERS; WINGS;

AERODYNAMIC PERFORMANCE; BLENDED WING BODY AIRCRAFT; PARALLEL EFFICIENCY; SHOCK CONTROL BUMPS;

AIRCRAFT;

EID: 34147134975     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000004425     Document Type: Article

References (17)

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