Publications

Detailed Information

겹침 격자 기법 기반의 매개 변수법을 이용한 항공기 형상 최적 설계 = Aerodynamic shape optimization using discrete adjoint approach on overset mesh system

Cited 0 time in Web of Science Cited 0 time in Scopus

Altmetrics

Item View & Download Count

  • mendeley

Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.

Share