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Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers
Aerodynamic shape optimization supersonic aircraft configurations via adjoint formulation distributed memory parallel computers
2015/7/1
This work describes the application of a control theory-based aero dynamic shape optimization method to the problem of supersonic aircraft design.
Computers and Aviation
Computers Aviation
2015/6/18
To trace the parallel development of computing and flight over the last
300 years, culminating in a fusion of engineering, mathematics and
computing in modern aviation.
“From Physics to Daily Life” Colloquium Computers and Aviation
From Physics to Daily Life Computers Aviation
2015/6/18
To trace the parallel development of computing and flight over the last
300 years, culminating in a fusion of engineering, mathematics and
computing in modern aviation.
