Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 2
Year: 1999
Type: article
Source: Journal of Aircraft
DOI: 10.2514/2.2414
Institutions: Ames Research Center, Stanford University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4248846264