비정렬 격자 기반 해석자 UMSAPv 검증 및 OPPAV 항공기 공력 해석

VALIDATION OF UNSTRUCTURED SOLVER UMSAPV AND AERODYNAMIC ANALYSIS OF FULL AIRCRAFT OPPAV

초록

UMSAPv is a newly developed three-dimensional unstructured node-based finite volume solver. The solver is validated for analyses of flows over various geometries, from the laminar flow over a sphere to the turbulent flows over a NACA0012 airfoil, an ONERA M6 wing, an RAE A wing-body, and a delta wing-cylindrical body. And the accuracy of the solver is examined by comparing its results with wind tunnel tests and results of others. In addition, It shows the high usability by being analyzing flows over an aircraft with complex geometry such as landing gear and pylon.

키워드

비정렬 격자 기반 해석자실험유체역학전산유체역학OPPAVUnstructured Mesh Based SolverEFDCFDOptionally Piloted Personal Air Vehicle
제목
비정렬 격자 기반 해석자 UMSAPv 검증 및 OPPAV 항공기 공력 해석
제목 (타언어)
VALIDATION OF UNSTRUCTURED SOLVER UMSAPV AND AERODYNAMIC ANALYSIS OF FULL AIRCRAFT OPPAV
저자
김광희백청이승수최재훈
DOI
10.6112/kscfe.2021.26.1.059
발행일
2021-03
유형
Y
저널명
한국전산유체공학회지
26
1
페이지
59 ~ 69